SES-16 (GovSat)

 2018-013A

---

At 21.5E, X/Ka-band military. Orbital ATK Geostar 3. SES military comms satellite for Luxembourg and NATO; LuxGovSat S.A. is a partnership between the Luxembourg government and SES.

The first stage tested a three-engine high thrust landing burn, and survived its impact with the water. The second stage reached a supersynchronous geotransfer orbit.

GovSat
Date	Time	Event	Orbit
2018 Jan 31	2125	Launch by Falcon 9	CC LC40
		T+2:38 MECO
		T+2:40 St 1 sep
		T+2:41 SEIG-1
		T+3:44 Fairing
		T+6:40? St 1 entry burn
		T+6:52 St 1 entry burn shutdown
		8:31 Landing burn, 3 engines
		8:42 St 1 splashdown
	2133	T+8:35 SECO-1
	2134	205 x 236 x 28.45
	2151	T+26:40 SEIG-2
	2152	T+27:48 SECO-2
	2157	T+32:19 Stage 2 sep	200? x 42000? x 26?

Elektro-L 2

 2015-074A

---

Elektro-L No. 2 (No. 1521) was somewhat more massive. After launch, several debris objects were found in the SBB orbit. The Fregat was no. 222-02 per NK, no. 2004 per other sources.

Bus can carry 570 kg prop.

Elektro-L
Date	Time	Event	Orbit
2015 Dec 11	1345:32	Launch by Zenit-3SLBF	KB LC45
		T+2:28 St 1 sep
		T+5:09 GO sep
		T+7:07 St 2 MECO
	1354:08	St 2 sep	164 x 539 x 51.4
	1500:07	MES-1
	1508:32	MECO-1
	1509:09	SBB sep	271 x 4277 x 50.4
	1711:50	MES-2
	1722:48	MECO-2	338 x 35911 x 48.6
	2232:08	MES-3
	2240:56	MECO-3
	2243:26	Fregat sep	35413 x 35785 x 0.5
2015 Dec 12		MES-4
		MECO-4
		Fregat disposal
2016 Jan 15			1435.46 35734 x 35813 x 0.4 GEO 77.5E

Hispasat 30W-6

 2018-023A

---

Loral 1300 . Originally Hispasat 1F. Replaces 1D/30W-4. Mass 6092 kg launch, 2623 kg dry, 730 kg BOL prop. Size 26.1m x 8.9m x 6.9m

30W-6
Date	Time	Event	Orbit
2018 Mar 6	0533:00	Launch by Falcon 9	CC LC40
		T+2:35 MECO
		T+2:37 St 1 sep
		T+2:39 St 2 burn
		T+3:39 Fairing
	0040	Entry burn St 1
	0042	Landing burn St 1
		Water impact St 1
	0541	T+8:39 SECO1
	0559	T+26:38 SEIG2
	0600	T+27:33 SECO2
	0605	T+32:51 Stage 2 sep
2018 Mar 6			387.34 189 x 22256 x 27.0
2018 Mar 6	0645?	Eject PODSAT
2018 Mar 7	1800?	Raise perigee
2018 Mar 7			388.59 284 x 22235 x 27.0
2018 Mar 9			448.54 296 x 25757 x 27.0
2018 Mar 10			528.35 308 x 30233 x 27.0
2018 Mar 12			636.73 317 x 35960 x 27.0
2018 Mar 13			739.68 5524 x 35905 x 13.8
2018 Mar 14			946.39 15246 x 35858 x 5.5
2018 Mar 14			1367.95 33114 x 35769 x 0.3
2018 Mar 16			1444.62 35788 x 36118 x 0.1 GEO 25.8W-2.1W

LKW-4

 2018-025A

---

Launched to 1330 LTDN SSO.

LKW
Date	Time	Event	Orbit
2018 Mar 17	0710	Launch by CZ-2D	JQ
	0720?	Stage 2 sep	490 x 502 x 97.3
	0728?	Stage 2 deorbit
	0754?	Stage 2 impact Antarctic?

Sex, Hair and Billionaires: The Adventures of a Celebrity Hairstylist

https://welib.org/md5/93ce1ba95950856501ff5ec460c99204

Rosetta-Philae

 2004-006A

---

Rosetta was launched by the first Ariane 5G+ in 2004. Rosetta was built by Astrium (formerly Daimler-Benz Aerospace's Dornier Satellitensysteme) of Freidrichshafen. The spacecraft is box-shaped with 2 solar wings, a propulsion system with 24 10N thrusters and a 2.2m dia HGA. Mass is 809 kg dry with 1720 kg of fuel (1060 kg N2O4 and 660 kg MMH).

2.8 x 2.1 x 2.0m box + 2 panels span 32m. Mass 3065 kg launch with 1670 kg of prop and a 100 kg lander.

Mass at EPC sep is 15708 kg (including full EPS). Mass at EPS burnout is 5892 kg implying a 2827 kg EPS mass at burnout but prior to passivation.

Rosetta will carry the German Surface Science Package (SSP) called Roland.

Rosetta was originally scheduled to carry the Champollion lander, but this was removed from the project in 1996.

Rosetta has Bus Support Module, Payload Support Module.

Control from ESOC.

Rosetta was prepared for launch in 2003 for a rendezvous with 46P/Wirtanen in 2011. After the 2002 Ariane 5 failure, Rosetta was postponed and redirected to 67P/Churyumov-Gerasimenko.

The vehicle was an AR5G+, which is an AR5G with the VEB from the AR5ES (100 kg lighter) and 250 kg extra prop in the EPS stage with an elongated MMH tank. Rosetta used an 123 kg 1194V5 EADS-CASA adapter on the EPS stage and the short A5 payload fairing (12.7m high 5.4m dia). The EPC is the standard AR5G type. The EAP boosters used a P2001 nozzle, 340 kg lighter than standard, pioneered on AR516.

21 Lutetia: 130 x 104 x 74 km, a=2.435 AU assume rho=2.2g/cm3 or 49 x 41 x 34 semiajor axes Albedo 0.1 to 0.2, taxonomy M, M0, W, Xk guesses largest asteroid visited to date. rot 8.17h C-type possible carbonaceous chrondrite type? (or M-type metallic?) But issues with albedo. IR featureless spectra High IR albedo; Lower radar albedo than any M-type asteroid. Hill radius 342Ra = 17111 km, critical distance from 166 to 332 Ra Stability surface (where orbiting objects could be found) in 215 x 361 x 361 Ra Solar radiation pressure perturbs small particles out; mm-size particles cleared, cm-sized particles remain.

Flyby 3055 km nominal

2867 Steins dia 5.5 to 17.5 km p = 6.05hr rot Type E (EII type like 64 Angelina, partial melts derived from enstatite chrondirtes) Iron-poor silicates on surface, like aubrite meteorites. Consistent with high albedo E-type = 0.45 ia 4.6 km.

Steins 1745 km 8.565 km/s

67P/C-G nucleus is 4.1km across, made of two lobes. THe large lobe is 4.1 x 3.2 x 1.3 km, the small lobe is 2.5 x 2.5 x 2.0 km. Rotation period is 12.4043 hours; mass is 1.0E13 kg.

 

Rosetta
Date	Time	Event	Orbit
2004 Mar 2	0717:44	Launch by Ariane 5 518G (V158)
		T+2:19 EAP sep
		T+3:11 Fairing sep
	0727:34	T+9:50 EPC burnout
	0727:40	T+9:56 EPC sep	45 x 3849 km x 5.67 deg
		Long coast for 1h45m
	0825	T+1:07:00 Apogee
	0914:29	T+1:56:45 L9.7 stage burn at 652 km
		T+2:05:06 Perigee at 225 km during burn
	0924?	Reentry of EPC
	0931:35	T+2:13:51 EPS MECO at 1097 km
		Vinf = 3.545 km/s
	0932:49	T+2:15:05 L9.7 sep	392 x -76662 x 5.70
	1757	Pass EL1:4
2004 Mar 3	1030	Pass lunar orbit
2004 Mar 3		TCM-1 1.0m/s
2004 Mar 5	0300	Leave Earth sphere
2004 Mar 6	2211	Leave Earth sphere 1.5Mkm
2004 Apr 26	0000		359.02d 0.8859AU x 1.0910AU x 0.41
2004 May 10		TCM-2 152.8m/s 3.5h
2004 May 14			365.33d 0.8864AU x 1.1137AU x 0.42
2004 May 16		TCM-3 5.0m/s
2004 Nov 25		TCM-4 0.17 m/s, anomaly
2004 Dec 9		TCM-5 0.12m/s
2005 Feb 8			365.11d 0.886 x 1.114 AU x 1.42
2005 Feb 17		TCM-6 0.09m/s
2005 Feb 28	1719	Enter Earth sphere 1.5Mkm
2005 Mar 2	0900	Enter SOI
2005 Mar 4	2209:14	Earth flyby 1955 km over Baja Cal.	1954 x -68130 x 144.9
2005 Mar 7	1115	Leave SOI
2005 Mar 9	0325	Depart Earth sphere 1.5Mkm
2005 Mar 28			588.42d 0.990 x 1.758 AU x 1.42
2006 May 23		Enter hibernation
2006 Jul		Begin Mars Swingby Phase
2006 Sep 29	0200	DSM-2 TCM-7 31.8m/s 52min
2006 Nov 13	2314	TCM-8 0.1m/s
2007 Feb 9	0200?	TCM-9 Mars-16d 54s 0.04m/s
2007 Feb 23	1543	Enter Mars sphere 1.08Mkm
2007 Feb 24	0740	Enter Mars SOI
2007 Feb 25	0145	Mars flyby 250 km	252 x -8152 x 136.3
2007 Feb 25	1950	Leave Mars SOI
2007 Feb 26	1148	Depart Mars sphere 1.08Mkm
2007 Apr 26		TCM-10 6.5m/s
2007 May 5			470.88d 0.784 x 1.585 AU x 1.90
2007		Asteroid belt
2007 Oct 18	1706	TCM 42s
2007 Nov 12	0109	Enter Earth sphere 1.5Mkm
2007 Nov 12	1800	Enter SOI
2007 Nov 13	2057	Earth flyby 2, 5301 km above 63 46S 74 35W	5299 x -27151 x 115.1
2007 Nov 15	0000	Leave SOI
2007 Nov 15	1650	Depart Earth sphere 1.5Mkm
2007 Dec 31			730.50d 0.911 x 2.264 AU x 7.71
2008 Sep 4	0856	TCM 0.12m/s
2008 Sep 5	1837:19	Enter Steins sphere
	1838:19	Flyby (2867) Steins at 803 km, 8.6 km/s
	1839:19	Depart Steins sphere
2009 Mar 18		DSM-4
2009 Oct 22	1526:10	TCM 1:27 0.09m/s 93 kg
2009 Nov 11	1155	Earth sphere 1.5Mkm
2009 Nov 12	0440	Earth sphere 0.9Mkm
2009 Nov 13	0745:40	Earth flyby 3, 2481 km
2009 Nov 14	1040	Leave Earth sphere
2009 Nov 15	0333	Leave Earth sphere 1.5Mkm
2009 Nov 26			1933.53d 0.980 x 5.094 AU x 4.38
2010 Jun 18	0624	TCM move aim from 2639 to 3169, 188s
2010 Jul 10	1512	Enter L sphere
	1544:55	Flyby (21) Lutetia at 3162 km at 15 km/s
	1620	Depart L sphere
2011 Jan 17	1903	OCM part 1
2011 Jan 17		OCM end. 301 m/s
2011 Jan 18	1859:13	OCM part 2, 274 m/s
2011 Jan 19	0113	OCM end
2011 Jan 21	s	OCM part 3
2011 Jan 23	s	OCM part 4
2011 Feb 1		2103.7d 1.136 x 5.290 AU x 6.58
2011 Jun 8		Hibernation
2014 Jan 20		Exit hibernation	2103.2d 1.134 x 5.290 AU x 6.58
2014 May 7	1730	Test burn 20m/s 45min
2014 May 21	1523	Orbit Match Mvr day 3140 300m/s
	2239	Burn complete
2014 Jun 4	1421:58	Burn 2, 6:39
	2100	Burn 2 complete, 190 kg prop
		Arrive at Churyumov-Gerasimenko
		Far Approach Phase
		Approach Transition Point
		Close Approach Phase
2014 Aug 2	0220	Enter CG Hill sphere
2014 Aug 6	0900	Close Approach Trajectory Insertion CATI 6:26 1m/s
		Rendezvous at 100 km, unbound
2014 Aug 10		100 km, CAT Change 1 TCM 6:25, 0.88 m/s, second 100 km leg
2014 Aug 11	2100	Closest approach 90 km
2014 Aug 13		100 km, CAT Change 2, 6:22, 0.87m/s, 3rd 100 km leg
2014 Aug 17	0900	100 km, CAT Change 3, 6:19, 0.85m/s, Transfer to 80 km
2014 Aug 19	0700	Closest approach 79 km
2014 Aug 20	0900	CAT 4, 92 km distance, burn to reduce height
2014 Aug 21	0230?	Within 79 km
2014 Aug 24	0900	At 72 km, CAT 5 ('little CAT')
2014 Aug 25		Below 60 km
2014 Aug 25		Close apporach at 52 km, arc 1
2014 Aug 27		At 72? km, CAT 6, leg 2
2014 Aug 29		Close apporach at 52 km, arc 2
2014 Aug 31		At 72? km, CAT 7,leg 3
2014 Sep 1		Close approach at 52 km, arc 3
2014 Sep 3	0900	At 72 km, TGM1 0.6m/s 4:55 Transfer to GMP
2014 Sep 7		TGM2 0.5m/s 04:18
2014 Sep 10		GMP1 0.2m/s 02:19
2014 Sep 10		Global mapping phase 30 km
2014 Sep 14		GMP slot1 0.03m/s 32s
2014 Sep 17		GMP-2A 0.09m/s 1:23
		GMP-2B 0.09m/s 1:25	28 x 29 km
2014 Sep 21		GMP slot 2 0.02m/s 25s
2014 Sep 24	s	burn
2014 Sep 24		Distance r=28.5 km	20 x 30
		Begin descent to 20 km
2014 Sep 29	0900	burn	20 x 20
2014 Oct 8	s	burn	10 x 20
2014 Oct 15	s	burn	10 x 10
		Close observation phase
2014 Oct 27?		8 x 10
2014 Oct 28	1259	Raise burn 82s, 0.08m/s	10 x 30
2014 Oct 31		Circ burn 90s	30 x 30
		SSP delivery phase
		Relay orbit phase
		Extended monitoring phase 200d?
		Perihelion at day 3800
2014 Nov 12		S-2h Pre-Sep manoeuvre
		Roland SSP delivery from 22.5 km radius
2014 Nov 14?		Move to 30 km orbit
2015 Feb 4		Move to unbound orbits for flybys
2015 Feb 4		Range 26 km
2015 Feb 7		Range 142 km apocomet
2015 Feb 11		Range 101 km
2015 Feb 14		Range 48 km
2015 Feb 14	0100	TCM
2015 Feb 14	1240:50	6 km alt flyby
2015 Feb 17		253 km
2015 Feb 20?		Flyby at about 20 km?
2015 Feb 25		76 km
2015 Mar 4		88 km
2014 Mar 7		88 km
2015 Mar		Philae end of life?
2015 Mar 28		14 km flyby
2015 Mar 28		Emergency avoid burn, range to 400 km
2015 Apr 1	0419	Pass 349 km Hill Sphere outbound
2015 Apr 1		TCM to brake
2015 Apr 4	0050	Max range at 385 km
2015 Apr 4		TCM on course for 140 km approach
2015 Apr 4	1412	Pass 344 km Hill Sphere inbound
2015 Apr 8		140 km approach
2015 Apr 11		100 km, pyramid path
2015 Apr 25		Range 93 km
2015 May 23		Range 138 km
2015 May 26	1256	Pass 276 km Hill Sphere outbound
2015 May 27	1354	Max range at 325 km
2015 May 28	1844	Pass 274 km Hill Sphere inbound
2015 Jun 1		Range 209 km
2015 Jun 5		Range 208 km
2015 Jul 1		Range 160 km
2015 Jul 3		Range 168 km
2015 Jul 6		Range 160 km
2015 Jul 7		Range 153 km
2015 Jul 12		Range 155 km
2015 Jul		Rosetta plume flythrough
2015 Jul 25		S hem observations from 180 km
2015 Jul 27		Range 170 km
2015 Jul 28		Range 197 km
2015 Jul 30		Range 179 km
2015 Aug 3	2130	Pass 221 km Hill Sphere outbound
2015 Aug 4		Range 222 km
2015 Aug 7		Range 283 km
2015 Aug 10		Range 317 km
2015 Aug 12		Range 334
2015 Aug 13		R over N hem, 325 km
2015 Aug 13		67P perihelion
2015 Aug 17		Range 328
2015 Aug 20		Range 325
2015 Aug 24		Range 365
2015 Aug 25		Range 418
2015 Aug 30		Range 404
2015 Sep 3		Range 383 km
2015 Sep 14		Range 317 km
2015 Sep 21		Range 329
2015 Sep 22		Range 340
2015 Sep 23		Begin far excursion trajectory
2015 Sep 23		Range 406
2015 Sep 24		Range 538
2015 Sep 26		Range 771
2015 Sep 28		Range 1115
2015 Sep 29		Range 1394
	2302	Range 1480
2015 Sep 30	0145	Range 1501 km, max range
2015 Sep 30	0602	Range 1490
	0945	Range 1468
	1125	Range 1459 km
	1258	Range 1451
2015 Oct 1		Range 1354
2015 Oct 2		Range 1128
2015 Oct 4		Range 928
2015 Oct 8		Range 616
2015 Oct 14		Range 495
2015 Oct 18		Range 432
2015 Oct 20		Range 422
2015 Oct 23		Range 370
2015 Oct 28		Range 295
2015 Nov 1	0853	Pass 278 km Hill Sphere inbound
2015 Nov 3		Range 263
2015 Nov 12		Range 174
2015 Nov 17		Range 144
2015 Nov 29		Range 122
2015 Dec		End of primary mission
2015 Dec 3		Range 100 km
2015 Dec 10		Range 99 km
2015 Dec 16		Range 112 km
2015 Dec 25		Range 75 km
2015 Dec 30		Range 88 km
2016 Jan		Comet activity declines, reapproach
2016 Jan 10		Range 79 km
2016 Jan 27		Range 72 km
2016 Jan 30		Range 61 km
2016 Feb 5		Range 53 km
2016 Feb 10		Range 49 km
2016 Feb 27		Range 30 km
2016 Mar 5		Range 20 km
2016 Mar 12		Range 17 km
2016 Mar 16		Range 14 km
2016 Mar 19		Range 12 km
2016 Mar 23		Range 37 km
2016 Mar		Anti-sunward excursion
2016 Mar 27		Range 329 km outbound
2016 Mar 28	0949	Pass 475 km Hill Sphere outbound
2016 Mar 29		Range 820 km
2016 Mar 30	1353	1000 km antisunward, max range
2016 Apr 2	1853	Pass 482 km Hill Sphere inbound
2016 Apr 3		Range 442 km
2016 Apr 9		Range 30 km, zero phase flyby
2016 Apr 10		Range 30 km
2016 Apr 13		Range 109 km
2016 Apr 21		Range 31 km
2016 Apr 23		Range 30 km
2016 Apr 29		Range 18 km
2016 May 3		Range 18 km
2016 May 11		Range 10 km
2016 May 25		Range 7 km
2016 May 28		Range 7 km
2016 May 29		Range 5 km, safemode
2016 May 30		Resume contact
2016 Jun 2		Transition to 30 km orbt
2016 Jun 4	0140	30 km orbit insertion
2016 Jun 7		Range 28 km
2016 Jun		N Hem mapping
2016 Jun 15		Range 34 km
2016 Jun 25		Range 18 km
2016 Jul 2		Range 17 km
2016 Jul 3		Range 9 km
2016 Jul 10		Range 10 km
2016 Jul 24		Range 10 km
2016 Aug 3		Range 9 km
2016 Aug 9		Flyover regime
2016 Aug 10		Range 13 km
2016 Aug 15		Range 7 km
2016 Aug 17		Range 14 km
2016 Aug 22		Range 7 km
2016 Aug 24		Range 9 km
2016 Aug 27		Range 5 km
2016 Aug 30		Range 4 km
2016 Aug 31		Range 9 km
2016 Sep 2		Range 2.7 km; Philae found
2016 Sep 5		Range 3.9 km flyover, 1.9 km height
2016 Sep 8		Range 4 km
2016 Sep 11		Range 10 km
2016 Sep 17	s	Flyover
2016 Sep 20	s	Flyover
2016 Sep 24		Post flyover burn
2016 Sep 26		Transfer burn	16 x 23 km
2016 Sep 29	2050	Deorbit burn 3 min, alt 19 km 0.34m/s
2016 Sep 30		Descent to Ma'at/Deir el-Medina
	0800?	Activate passivation commands; 100 kg prop left
	1039:34	Touchdown at Sais, 0.9m/s
	1119	LOS at ESOC

Payload:

• OSIRIS Multicolor imaging with narrow, wide angle cameras

• ALICE UV spectroscopy 700-2050 A

• VIRTIS Vis/IR mapping spectroscopy 0.25-5 mu

• MIRO Microwave spectroscopy 1.3, 0.5mm

• ROSINA Neutral gas, ion mass spectroscopy

• MODULUS Gas chromatograph for light elements

• COSIMA Dust mass spectrometer

• MIDAS Atomic force microscope for grain morphology

• CONSERT Radio sounding comet nucleus tomography

• GIADA Dust flux,velocity/momentum, contamination monitor

• RPC Comet plasma:

  • Langmuir probe

  • Ion/electron sensor

  • Flux gate magnetometer

  • Ion composition analyser

  • Mutual impedance probe

• RSI Radio science experiment

2004-006

---

The Rosetta Lander (RoLand) will be deployed onto the comet's surface. The lander was named Philae after the location of an obelisk which helped Champollion decipher the Rosetta stone. Some of the experiments are also carried on the orbiter. Lander is 85 kg, of which 21 kg are experiments.

Size is box + half octagon, 0.9 x 0.9m, with 2.0m span across legs. OWLT is 00:28:20 at 511 million km.

The selected landing site was Site J, subsequently named Agilkia, after the Nile island which now houses the relocated Philae temple complex. After bouncing twice, Philae landed at another site later named Abydos.

Philae
Date	Time	Event	Orbit
2014 Nov 11	1805	Switchon
	2024	Lander flywheel on
2014 Nov 12	0335	Sep Descent and Landing (SDL) sequence on
	0735	Rosetta pre-sep mvr to comet-hyperbolic orbit
	0835	Philae sep from Rosetta at 0.18m/s, range 22.5 km
	0844	100m range, deploy landing gear
	0856:20	Deploy ROMAP boom
	0857	Rotation to stable landing orientation
	0915	Post delivery mvr
	1025	AOS Philae-Rosetta signal sent
	1053	AOS detected on Earth
	1534	Landing at 1m/s
		Fire harpoons, failed
		Flywheel off
	1534	Bounce to 70 m?
	1620	Hit surface, tumbled
		Reached 170m height
	1726	Second touchdown, bounce
	1732	Third touchdown, Abydos
2014 Nov 14	0930	LOS
2014 Nov 14	2251	AOS
2014 Nov 15	0008	Philae in hibernation, LOS
2015 Jun 14		Signal from Philae received
2015 Jul 9		Last pre-perihelion signal from Philae

Payload:

• ROLIS Roland Imaging System

• CONSERT Comet nucleus sounding experiment by Radiowave Transmission

• SESAME Surface electrical sounding and acoustic monitoring experiment, dust impact monitor; mechanical and electrical parameters

• APXS Alpha p/X-ray spectrometer

• MUPUS Multi-purpose sensor for surface and sub-surface science

• ROMAP Roland magnetometer and plasma monitor

• CIVA Comet nucleus infrared and visible analyser (cameras,s spectrometer for surface samples)

• SD2 Sampling, Drilling and Distribution instrument (drill, depth 23 cm)

• COSAC Cometary Sampling and Composition Experiment, looking for organic molecules

SES-15

 2017-026A

---

Boeing electric-propulsion 702SP for Ku/Ka-band over N AMerica and in-flight wifi; widebeam and high throughput. Opens a new SES location at 129W for N American coverage. Launch by Ariane. Mass 2302 kg, size 6 x 3 x 2m box + 2 panels.

SES15
Date	Time	Event	Orbit
2017 May 18	1154:53	Launch by Soyuz ST-A/Fregat	CSG
		T+1:58 Boosters sep
	T+3:39 Fairing sep
		T+4:47 Blok A sep
		Blok I MECO
	1203:42	T+8:49 Blok I sep	-764 x 200 x 6.32
	1204:42	T+9:49 MES-1
	1218:27	T+23:34 MECO-1	284 x 31431 x 6.06
	1652:28	T+4:57:35 MES-2
	1653:20	T+4:58:27 MECO-2	2200 x 31300 x 6.00
	1713:21	T+5:18:28 Fregat sep
		MES-3
		MECO-3	2341 x 31312 x 6.21
2017 May 20			584.01 2215 x 31316 x 5.9
2017 May 30			593.37 3181 x 30843 x 5.3
2017 Jun 29			762.36 5879 x 36652 x 3.9
2017 Jul 26			934.56 9578 x 40993 x 3.0
2017 Aug 16			1080.25 13152 x 43840 x 2.3
2017 Sep 6			1184.77 17401 x 44021 x 1.7
2017 Sep 20			1265.30 21161 x 43585 x 1.4
2017 Oct 10			1312.58 25007 x 41658 x 1.0
2017 Oct 25			1365.14 29410 x 39362 x 0.6
2017 Nov 4			1383.15 32061 x 37426 x 0.3
2017 Nov 17			1425.45 35409 x 35750 x 0.0
2017 Nov 20		Move in 137W
2017 Nov 24			1436.12 35783 x 35789 x 0.0 GEO 137.0W

STS-123 (Endeavour)

 2008-009A

---

122364 kg launch, 94157 kg landing.

EMU 3004 (Linnehan) and 3003 (Foreman, Behnken) will be left on ISS, and EMU 3006 and 3008 will be returned.

EVA1: EV4 Reisman 3006, EV1 Linnehan 3004

Prep JLP for unberth, install OTCM on SPDM and prep SPDM. JEM ELM-PS to Node 2 zenith.

EVA2: EV1 Linnehan 3004, EV3 Foreman 3003

Deploy SPDM in bay.

EVA3: EV2 Behnken 3008, EV1 Linnehan 3004

Install OTP and THA on SPDM, install CLPA, transfer LWAPA to COL-EPF, install MISSE 6, transfer Yaw Joint and DCSU 1/2 to ESP-2.

LWAPA goes on the nadir EPF (SDN) and MISSE 6 PEC 6a/6b are attached to it.

EVA4: Foreman 3008, Behnken 3003

S0 RPCM repair, Z1 reconfig, T-RAD DTO.

EVA5: Foreman 3008, Behnken 3003

Install OBSS KAU; OBSS transfer to S1, SARJ TBA-5 install

Contingency: Linnehan 3006, Foreman 3008

Total cargo up 17048 kg. Cargo left in space: Dextre, ELM-PS, 3 ORUs, and 2 MISSE PEC for a total of 10974 kg; MISSE LWAPA and OBSS puts it up to 11456 kg, so cargo down 5592.

Cargo STS to ISS outside: 10785 kg including 8336 kg ELM and 1556 kg Dextre, 893 kg other (not including OBSS?) inside: 650 kg plus 286 kg consumables. ISS to MD, 710 kg. MD cargo includes two EMU up and down and a 5 kg RPCM down.

STS-123
Date	Time	Event	Orbit
2007 Aug		Begin processing in OPF/2
2008 Feb 11		Tow to VAB
2008 Mar 11	0628:14	Launch
	0630:18	SRB sep
	0630:29	OMS ASS
	0632:23	OMS ASS CO
	0636:37	MECO	87.34 56 x 229 x 51.6
	0636:59	ET sep
	0706:44	OMS-2
	0707:47	OMS-2 CO
	0823:02	PLBD open	89.16 177 x 288 x 51.6
	0937:37	OMS-3 NC1 burn	89.17 179 x 287 x 51.6
	0938:26	OMS-3 CO
	2334:44	OMS-4 R
	2335:01	OMS-4 CO
2008 Mar 12			89.28 190 x 287 x 51.6
	2211:09	OMS-5 NH burn	89.29 193 x 284 x 51.6
	2212:05	OMS-5 CO
	2310:32	NC4 OMS-6 both, 112693 kg
	2311:31	OMS-6 CO
	2347?	NCC
2008 Mar 13
	0042:22	TI OMS-7 L 111642 kg 2.8 m/s
	0042:33	OMS-7 CO
	0105	MC1
		MC2
	0154	MC3
	0204	MC4, 520m
	0220	200m below station
	0235	RPM complete
	0240	Begin flyaround from +Rbar to Vbar
	0258	On +Vbar at 114m
	0300	Begin approach on Vbar
	0315	60m
	0325	40m
	0337	20m
	0349:48	Docking	91.35 339 x 341 x 51.6
	0537	HO
	0700?	SSRMS grapple SLP
	0730?	SLP unberthed	91.35 339 x 341 x 51.6
	0746	SLP in motion
	0750	Reisman seat liner on Soyuz; crew swap
	0800?	SLP berthed on truss POA on MBS
	0820?	SSRMS ungrapple SLP
2008 Mar 14
		EVA-1 Reisman, Linnehan
	0100	Begin depress
	0104	2.0 psi
	0108	Pressure 1 psi
	0113	0.7 psi
	0118	HO
	0118	Battery power
	0126	Egress Linnehan
	0144	Egress Reisman
	0300	Complete JLP prep
	0322	SRMS grapple JLP
	0400	Working on SLP
	0506	OCTM-2 attached to Dextre
	0632	JLP latches open
	0634	JLP unberthed by RMS
	0747?	Ingress Reisman
	0801	Ingress Linnehan
	0802?	TC
	0804	JLP RTL on Node 2
	0806	JLP berthed on Harmony zenith
	0814	HC
	0819	Repress
	2257	JLP power OK
	2349	SSRMS grapple OBSS
2008 Mar 15	0013	OBSS grapple by SRMS
	0038	OBSS ungrapple by SSRMS
	0125	HO to JLP, ingress
	0202	SSRMS grapple SPDM	91.35 339 x 341 x 51.6
	0210	SPDM has power
		EVA-2 Linnehan, Foreman
	2343	Depress 0.7
	2348?	HO
	2349	BP
2008 Mar 16	0000?	Egress Linnehan
	0005	Egress Foreman
	0230?	Arm 1 unberthed
	0255	Arm 1 on temp SLP stow
	0353	Arm 2 unberthed
	0450	Arm 2 on SPDM
	0500	Arm 1 off temp stwow
	0510	Arm 2 on SPDM
		SPDM assembly
	0610	Foreman returning to Quest
	0621	Foreman ingress?
	0631	Linnehan to CETA cart to stow APFR
	0638	Foreman inside airlock
	0647	Linnehan ingress
	0647	TC closed
	0654	HC
	0657	Repress
	s	SSRMS grapple SPDM
2008 Mar 17		EVA-3
	2227	7 psi
	2231	5 psi, pause
	2237	2 psi, pause
	2244	Below 1 psi
	2246?	Depress
	2248	0.5 psi
	2251	HO
	2251	Battery power
	2300?	Behnken egress
	2305	Linnehan egress
	2348	Working on SLP at MBS
2008 Mar 18
	0040?	OTP unberth
	0116	Completed OTP SPDM tool platform install
	0154	Linnehan retrieving LWAPA
	0159	LWAPA unberthed
	0206	Carrying LWAPA to COL EPF	91.35 340 x 341 x 51.6
	0222	LWAPA installed on COL EPF
	0240	Linnehan at Yaw Joint
	0246	YJ unberthed
	0304	YJ on esp2
	0313	Linnehan leaving esp2
	0330	Linnehan unberthed dcsu
	0340?	MISSE 6bunberthed by Behnken
	0350?	DCSU at ESP2
	0354	MISSE PEC 6b near LWAPA by Behnken
		Problems installing PEC
	0412	DCSU-2 unberthed by Linnenhan
	0423	Abandon attempts to install PEC
	0450?	MISSE PEC returned to PLB
	0508	Cleanup
	0527	Linnehan ingress
	0536	Behnken ingress
	0541	HC
	0545	Repress (NASA 6:53)
	0615?	SSRMS grapple SPDM
	0730?	SPDM on SSRMS out of SLP
	1955	SPDM grapple contact with Destiny
	2000	SPDM grappled PDGF on Destiny
	2124	SPDM based on Destiny
2008 Mar 19	0140	SSRMS ungrapple SPDM
	0220	SSRMS grapple SLP
	0240?	SLP unberthed from P1 POA
	0352	SLP keel latch in PLB
	0354	SLP berthed
	0402	SSRMS ungrapple SLP
2008 Mar 20	2135	Depress underway
		EVA-4 Foreman, Behnken
	2156	1.0 psi
	2159	Depress
	2200	0.6 psi
	2203	Go for HO
	2203	HO?
	2204	Battery power
	2211	Egress Behnken
	2222	Egress Foreman
	2245	broken RPCM removed from S0 truss
	2300	Failed to fix connector on Z1
	2320	Prep for T-RAD DTO
2008 Mar 21
	0200	T-RAD complete
	0245	Stowing T-RAD eqpt
	0414	Ingress Foreman
	0417	Ingress Behnken
	0418	TC closed
	0425	HC
	0428	Repress
		Transfer Expr3 from Destiny to Col
	2000?	OBSS on SRMS for survey
2008 Mar 22
		EVA-5 Foreman, Behnken
	2024	2 psi
	2028	1 psi
	2029	0.8 psi
	2030	DEPRESS
	2030	0.6 psi
	2032	0.5 psi
	2034	HO
	2034	BP
	2040	Foreman egress
	2046	Go to grapple OBSS
	2047	Behnken egress
	2051	Grapple OBSS with SSRMS
	2102	SRMS ungrapple OBSS
	2125	Avionics box installed on truss
	2220	OBSS nearly on truss
	2232	SSRMS ungrapple OBSS, in EV hands
	2241	OBSS soft docked to S1 truss
	2330	SARJ inspection
	2339?	MISSE PEC unberthed
2008 Mar 23	0000?	MISSE PEC6a installed?	91.35 340 x 341 x 51.6
	0010?	MISSE PEC unberthed
	0027	MISSE PEC installed on LWAPA
	0145	Thermal covers on JLP trunnions
	0145	SARJ inspection complete
	0221	ingress
	0226	ingress complete
	0227	tc
	0231	HC
	0236	Repress
2008 Mar 24
	2149	HC to ISS
2008 Mar 25
	0025:01	Undocking
	0043	250 ft
	0044	347 ft
	0048	425 ft
	0052	begin flyaround
	0102	zenith
	0115	behind
	0123	nadir
	0136	sep1
	0204	sep2	91.36 340 x 342 x 51.6
	1753s	OMS adjust	91.41 341 x 346 x 51.6
2008 Mar 26
	1923:49	PLBD closed	91.41 341 x 346 x 51.6
	2333:14	OMS DO 2:45 92.0m/s	42 x 352
	2335:59	OMS DO CO
2008 Mar 27	0007:29	EI
	0039:08	15:18:10:54 MGTD KSC RW15
	0039:17	NGTD
	0040:41	WS