Globalstar 60

 2000-008A

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Globalstar 60, 62 63 and 64 completed the constellation with MS-7. Each satellite weighed 448 kg for a total of 1792 kg. M060 remained in parking orbit through mid 2000.

Globalstar 60
Date	Time	Event	Orbit
2000 Feb 8	2124:00	Launch by Delta 7420-10	CCAFS SLC-17B
		T+1:03 SRM 1-4 burnout
		T+1:07 SRM 1-4 sep
		T+4:24 MECO
		T+4:32 St 1 sep
		T+4:37 SES-1
		T+4:47 Fairing sep
	2135	T+11:18 SECO-1	185 x 914 x 51.9
		T+1:02:13 SES-2
		T+1:02:32 SECO-2	916 x 916 x 52.0
	2231	T+1:07:03 U1/U2 sep
	2235	T+1:11:16 L1/L2 sep
		T+01:44:23 SES-3
		T+01:44:28 SECO-3
		T+01:51:53 SES-4
		T+01:52:18 SECO-4
2000 May 27			103.46 910 x 934 x 52.0
2005 Jul 18			114.08 1411 x 141 x 52.0

Kompass

 2006-019A

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Complex Orbital Magneto-Plasma Autonomous Small Satellite

(possibly: Kompleksniy Orbital'niy Magnito-Plazmenniy Avtonomniy Sputnik; not confirmed)

Launch by RSM-54 Shtil'.

Truncated prism + 2 panel + booms. 0.5m dia 1.0? m long 3?m span. Mass 80 kg. Plan 400-500 x 620 km x 79 deg.

Launch by Ekaterinburg K-84 in submerged position. The satellite initially failed, but was reactivated in Dec 2006.

Kompass
Date	Time	Event	Orbit
2006 May 26	1850	Launch by Shtil'
		Stage 1 burn
	1851:15	T+1:15 Stage 1 Sep 30 km	-6300? x 60? x 78.9
		T+1:15 Interstage halves sep
	1851:15	Stage 2 burn
	1852:49	T+2:49 Stage 2 sep 109 km	-5200? x 160? x 78.9
		T+2:49 Mode A start, Stage 3 MES 109 km
	1854:16	T+4:16 Mode M start 174 km, Stage 3 MECO	-1650? x 400 x 78.9
	1855:20	T+5:20 Stage 3 engine sep 224 km; impact Pacific	-1620? x 400 x 78.9
	1900:41	T+10:41 B mode, Apogee leg begins, BR MES 800 m/s?	-1500? x 400 x 78.9
	1905:06	T+15:06 Apogee leg ends, BR MECO	400 x 700? x 78.9
		BR in low thrust mode
	1905:11	T+15:11 Payload capsule sep from nosecone	400 x 710? x 78.9
	1905:47	T+15:47 Payload capsule cover ejected
	1905:47	T+15:47 Payload ejected from capsule at 2.2m/s
	1905:47	T+15:47 Nosecone thrust off, 100m away
		Stage 2 impact 85E 78N
	1913?	Stage 3 engine impact Pacific range 9052 km, 173E 25N?
2006 May		Transmitter failed?
2006 Dec		Reactivated

Payload:

• PES Total electron content, plasma concentration

• MAYAK Ionospheric vertical profile, electron concentration over seismo-active regions

• RFA Radio frequency analyser 100 kHz - 15.1 MHz E fields

• NVK Low frequency UHF/VHF wave burns, links between seismic activity and electromagnetic fields

Aviation Week: June 18,2007

 https://welib.org/md5/8423b30723d6280a4e3e131fd04f562a

Eurobird 1

 2001-011A

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Eutelsat's Eurobird satellite, originally Eutelsat W1, is a Spacebus 3000B2. The first W1 was destroyed in a ground fire at Cannes on 1998 May 18 and declared a launch. A new Eutelsat W1 was then built, to be launched in 2000 to 28E. It was renamed Eurobird when Ressat became the new W1 in 2000.

Launch mass is 3050 kg. Size is 3.5 x 3.4 x 2.3m with 29m span.

Eurobird
Date	Time	Event	Orbit
2001 Mar 8	2251	Launch by Ariane 5G	CSG ELA3
		T+2:25 EAP sep
		T+3:14 Fairing sep
		T+9:40 EPC MECO
	2300	T+9:46 EPC sep
	2300	T+9:53 EPS burn
	2317	T+26:37 EPS MECO
	2320	T+29:13 Eurobird sep
	2323	T+32:29 Sylda 5 sep
	2327	T+36:21 BSAT-2a sep
2001 Mar 8		647.44 919 x 35906 x 2.3
2001 Mar 8	1700?	LAM-1
2001 Mar 12			1352.43 32467 x 35797 x 0.3
2001 Mar 14	0950?	LAM-2
2001 Mar 14			1386.22 33798 x 35810 x 0.2
2001 Mar 15	0800?	LAM-3
2001 Mar 16			1436.24 35768 x 35810 x 0.1 GEO 32.4E+0.04W
2001 Apr 6			1436.05 35781 x 35790 x 0.1 GEO 28.5E
2006 Aug 1			1436.09 35773 x 35799 x 0.1 GEO 28.5E