Globalstar 79

 2010-054A

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The second generation Globalstar consisted of 48 sats from Alcatel Alenia Space/Roma (payloads in Toulouse, structures in Cannes, assembly and integration in Roma). 715 kg each. Approx size Trapezoid 4 x 2 x 1m? +panels? Six sats on first launch (FM2 to 7?)

Based on the Proteus/Spacebus-L500 bus. Conical dispenser 550 kg Astrium-AELM In 2011 UN responsibility for these Globalstar satellites was transferred to France.

Fregat/Globalstar injection mass is 8200 kg at -974? x 200 x 51.7 (Vi = 7.393 km/s)

Globalstar
Date	Time	Event	Orbit
2010 Oct 19	1710	Launch by Soyuz-2-1A/Fregat 009/1023	KB LC31/6
		T+1:58 Strapons sep
		T+4:47 Blok A sep
		T+4:56 KhO sep
		T+4:58 ST Fairing sep
	1718	T+8:45? Blok I MECO
	1718	T+8:49 Blok I Sep	-974? x 200 x 51.7
	1719?	T+9:49? Fregat MES-1
	1723	T+13:18 Burn in progress
	1725?	Fregat MECO-1	210 x 923 x 51.7
	1732	T+22:54 In coast
		50 min coast
	1813?	T+1:03? Fregat MES-2
	?	Fregat MECO-2	920 x 920 x 52.0
	1848	T+1:38:40 Sat 1-2 sep, upper deck
	1850	T+1:40:20 Sat 3-6 sep, lower deck
2010 Oct 19	1900?	Fregat deorbit over S Pacific
		Fregat DO CO	79 x 929 x 52.0
	1948?	Fregat reentry
2010 Oct 21			920 x 920 x 52.0

Kosmos 2469

 2010-049A

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Oko launches continued in 2010 with Kosmos-2469. It was reported to be the hundredth and last in the series.

Oko
Date	Time	Event	Orbit
2010 Sep 30	1701	Launch by Molniya-M/2BL	PL LC16/2
	1710	Blok-I MECO
	1710	Blok I sep
	1751?	Blok L burn
	1755?	Blok L MECO	92.06 226 x 524 x 62.8
	1757	Blok-L sep
	1846	AOS
2010 Oct 2			704.34 558 x 39130 x 62.8

Progress M-07M

 2010-044A

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Flight 39P. 11F615A60 No. 407. Launch mass 7122 kg. Cargo 2290 kg including 870 kg prop. 50 kg O2/air, 170 kg H20, 1200 kg parts and hardware, including 87 kg URM-D. Undocking mass 5503 kg. 

Progress M-07M
Date	Time	Event	Orbit
2010 Sep 10	1022:57	Launch by Soyuz-U	KB PL5/1
	1031:43	T+8:46 Blok-I MECO
	1031:46	Sep from Blok I
	1407:38	SKD DV1 51s 20.5m/s
	1455:30	SKD DV2 37s 14.8m/s (1+2 used 96 kg)
2010 Sep 11	1124:43	DPO DV3 26s 1.7s 10 kg
2010 Sep 12	1040	DV SKD
	1121	SKD DV 6.4m/s
	1126	DPO braking
	1130	400m range, flyaround
	1138	Lined up with SM
	1157:57	Docked with Zvezda
2010 Sep 15	0904	DPO burn reboost 8:46 1.3m/s, phasing for 22S landing
2010 Oct 25	1425:01	DPO burn, reboost 0.6m/s
2010 Nov 25	0503	SKD burn DV7:38 0.92m/s
2011 Feb 9	2137:30	reboost burn 251s 0,5m/s
2011 Feb 20	1311:47	Undocked
	1314:48	Sep burn 15s
	1612:00	Deorbit 2:34 87.5 m/s
	1614:34	Deorbit cutoff
	1658	Debris impact 42 30S 139 24W

Chollian

 2010-032A

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COMS, KARI's first multi-function geosat, built by EADS Astrium using Eurostar E3000. Carries experimental comms, oceaongraphy and meteorology payloads. 2461 kg at launch. Will be at 128.3 E.

COMS is the Communications, Oceanography and Meteorology Satellite. It was named

Clairvoyance, which may be transliterated 'Cheonlian' but which the Koreans render as 'Chollian' in English.

2.6 x 1.8 x 2.8m box + 1 panel. 17.2m span. Other side from panel has radiant cooler for MI.

Launch 2009 Ariane 5 CSG.

COMS
Date	Time	Event	Orbit
2010 Jun 26	2141	Launch by Ariane 5ECA L552 V195	CSG ELA3
		T+2:13 SRB sep
		T+3:02 Fairing sep
	2149	T+8:48 EPC MECO
		T+8:54 EPC sep	-1106 x 212 x 7.2
		T+8:58 ESC-A TIG
	2205	T+24:33 ESC-A MECO
	2207	T+26:32 Arabsat sep
	2211	T+30:04 Sylda 5 sep
	2213	T+32:31 COMS sep
2010 Jun 27			632.91 260 x 35820 x 2.0
2010 Jun 28			632.89 264 x 35815 x 2.0
2010 Jul 7			1436.10 35782 x 35790 x 0.0 GEO 128.2E
2010 Jul 13			1436.12 35785 x 35788 x 0.0 GEO 128.2E
2011 Mar 7			1436.08 35783 x 35789 x 0.0 GEO 128.2E
2011 Mar 8		Orbit adjust

Payload (communications):

• 28 C-band

• 24 Ku-band

• two C-band 2.2m dia dishes

• Ku-band global 2.4m dia beam

• Ku-band East/central 2.2m dia

• Ku-band West 1.5 x 1.3m beam

Payload (weather):

• SATCOM Korean Ka-band comms payload, 3 regional beams.

• MI Multi-spectral meteo imager, 4 IR channels with 4 km res and one vis channel with 1 km res.

• GOCI Ocean color imager - 8 visible bands with 0.5 km res.

• Weather data dissemination payload; L-band rx/S-band tx