Resourcesat 2

 2011-015A

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Launch with Youthsat and X-sat.

R2
Date	Time	Event	Orbit
2011 Apr 20	0442	Launch by PSLV-C16	SHAR FLP
		T+0:25 2km PSOM air on
		T+0:50 PSOM ground off
		T+1:07 23 km PSOM ground sep
		T+1:15 PSOM air off
		T+1:30 41km PSOM air sep
		T+1:47 PS1 MECO
		T+1:52 PS1 sep
		T+1:53 PS2 burn, 67 km, 1.97 km/s
		T+3:04 Fairing sep, 117 km 2.24km/s
	0446	T+4:24 PS2 MECO
		T+4:25 PS2 sep
		T+4:26 PS3 burn
		T+6:22 PS3 MECO
	0450	T+8:39 PS3 sep 601 km 5.665 km/s
	0450	T+8:50 PS4 burn 612 km 5.648 km/s
	0501	T+17:22 PS4 MECO
	0502	T+18:00 Resourcesat sep
		T+18:45 Youthsat sep
	0502	T+18:45 X-Sat sep
2011 Apr 22	0544?	Orbit raise

Payload:

• LISS-4 LISS-4 imager green, red, NIR, 70 km swath, 6m res

• LISS-3 imager, 23m medium res VNIR, SWIR

• AWIFS AWIFS-A and B cameras, 740 km swath, 56m res (3 bands VNIR, 1 band SWIR)

Worldview 2

 2009-055A

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Digital Globe's WV-2 satellite was launched in 2009, with an eight-band imager. BCP-5000 satellite.

It is 4.3m high 2.5m dia and 7.1m span with a mass of 2615 kg.

WV-2
Date	Time	Event	Orbit
2009 Oct 8	1851	Launch by Delta 7920	V SLC2W
		T+1:04 SRM 1-6 out
		T+1:05 SRM 7-9 on
		T+1:26 SRM 1-6 sep
		T+1:30 Dogleg
		T+2:09 SRM 7-9 out
		T+2:11 SRM 7-9 sep
		T+2:22 Dogleg end
		T+4:23 MECO
		T+4:31 St 1 sep
		T+4:37 SEIG-1
		T+4:41 Fairing sep
	1901	T+10:52 SECO-1	195 x 805 x 98.6
		T+53:34 SEIG-2 22s
	1944	T+53:56 SECO-2	764 x 776 x 98.6
		T+1:00:30 spinup
	1952	T+1:01:40 Stage 2 sep over Malindi
		T+1:11:40 cold gas evasive 0.4m/s 25s
		T+1:12:05 end evasive
		T+1:30:00 SEIG-3 evasive 5s over Thule
		T+1:30:05 SECO-3	333 x 759 x 98.66
		T+1:38:20 SEIG-4 depletion 51s over Hawaii
		T+1:39:11 SECO-4	217 x 752 x 92.41

Seventeen: September 2011

 https://welib.org/md5/9a9fb05478f69bf5508281a94a1cce96

Kosmos 2428

 2007-029A

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Zenit-2 No. 21L was modified to Zenit-2M No. 1-2005. The payload was a Tselina-2 satellite.

Kosmos-2428
Date	Time	Event	Orbit
2007 Jun 29	1000:00	Launch by Zenit-2M	KB LC45
	1002	T+2:23 St 1 MECO
	1002	T+2:25 Stage 1 sep
	1002	T+2:25 Stage 2 burn
	1002	T+2:40 GO sep
	1006	T+6:42 Stage 2 MECO	150? x 850? x 71.0
		Sep motor cover perigee
	1013?	T+13m? Stage 2 VECO
	1013?	Stage 2 sep motor covers
	1013:51	Stage 2 sep
2007 Jun 30			101.96 846 x 856 x 71.0

Chinasat 1A

 2011-047A

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Zhongxing 1A, built by CAST, was a second generation military comms satellite in the Feng Huo system.

Two slightly different timelines are given, one from launch coverage and the second a generic one from the CALT website.

ZX
Date	Time	Event	Orbit
2011 Sep 18	1633:03	Launch by CZ-3BE	XSC
		T+2:21 / 2:07 Boosters sep
		T+2:39 / 2:27 St 1 sep
		T+3:55 / 3:52 Fairing sep
		T+5:44 / 5:32 St 2 sep, St 3 MES-1
	1643	T+10:20 / 10:31 St 3 MECO-1
		T+21:04 / 21:21 MES-2
		T+24:00 / MECO-2
		T+24:20 VECO-2
	1658	T+25:40 / 25:59 St 3 sep	186 x 35818 x 27.1

Kosmos 2415

 2005-034A

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Kometa No. 21 flew a 44 day mission to complete the series.

Kosmos-2415
Date	Time	Event	Orbit
2005 Sep 2	0950	Launch by Soyuz	KB LC31
	0958	Blok I sep	196 x 285 x 64.9
2005 Sep 3		Orbit raise	205 x 284 x 64.9
2005 Sep 8			201 x 280 x 64.9
2005 Sep 15		Apogee raise
2005 Sep 21		Apogee raise	197 x 288 x 64.9
2005 Sep 27			195 x 281 x 64.9
2005 Sep 27		Perigee raise	203 x 278 x 64.9
2005 Oct 6		Perigee raise	206 x 268 x 64.9
2005 Oct 7			205 x 276 x 64.9
2005 Oct 13			204 x 269 x 64.9
		Apogee raise	204 x 311 x 64.9
2005 Oct 15			204 x 309 x 64.9
	2144	Landing after 43.5d
2005 Oct 16	0345	58E 55N southbound rev 706
	0520	55E 39N southbound rev 707
	1655	105E 41N northbound rev 715
	1825	84E 42N northbound rev 716
	1950	62E 43N northbound rev 717
	2112?	Deorbit over 17E 0S
	2128	51E 53N northbound rev 718
	2135?	Landing