Flock-2b 1-14

US

Spacecraft nº:

US spacecraft nº:


Launch data:

Designation (see table)
Launch date 19 Aug 2015 - 11:50 UT
Launch site Tanegashima, YLP-2
Launch vehicle  H-2B-304
Mission Imaging
Earth orbit: (see table)

Launched together with: HTV-5 - SERPENS - S-Cube - GOMX 3 - AAUSAT 5

Spacecraft data:

Prime manufacturer Planet Labs
Platform CubeSat (3U)
Operator Planet Labs
Mass at launch  5 kg
Dry Mass  kg
Basic shape  
Dimension (m) 
Equipment Solar cells
Stabilization  
Propulsion None
DC power  
Design lifetime  

 Flock-2b 1Flock-2b 2Flock-2b 3Flock-2b 4Flock-2b 5Flock-2b 6Flock-2b 7
Norad ID 40950 40951 40952 40953 40954 40955 40956
Int. code 98067HB 98067HC 98067HD 98067HE 98067HF 98067HG 98067HH
Deployment date 6 Oct 2015 - 01:15 6 Oct 2015 - 01:15 6 Oct 2015 - 04:30 6 Oct 2015 - 04:30 6 Oct 2015 - 08:31 6 Oct 2015 - 08:31 6 Oct 2015 - 11:45
Earth orbit
Perigee / Apogee 400x404 km 398x406 km 399x405 km 401x403 km 396x409 km 396x409 km 396x408 km
Inclination 51.6 deg 51.6 deg 51.6 deg 51.6 deg 51.6 deg 51.6 deg 51.6 deg
Period  min  min  min  min  min  min  min
Decay 22 Sep 2016 (.0) 02 Oct 2016(.78) 14 Oct 2016 (.4) 17 Oct 2016 (.35) 25 Sep 2016 (.7) 22 Aug 2016 21 Sep 2016 (.4)

 Flock-2b 8Flock-2b 9Flock-2b 10Flock-2b 11Flock-2b 12Flock-2b 13Flock-2b 14
Norad ID 40957 40958? 40959? 11 12 40979 40980
Int. code 98067HJ 98067HL 98067HK   98067HM 98067HN
Deployment date 6 Oct 2015 - 11:45 7 Oct 2015 - 00:10 7 Oct 2015 - 00:10 11 12 7 Oct 2015 - 12:25 7 Oct 2015 - 12:25
Earth orbit
Perigee / Apogee 397x408 km 397x408 km 397x408 km 11 km 12 km 395x408 km 396x408 km
Inclination 51.6 deg 51.6 deg 51.6 deg  deg  deg 51.7 deg 51.7 deg
Period  min  min  min  min  min  min  min
Decay 22 May 2016 (.33) 16 Oct 2016 (.56) 12 Oct 2016 (.0) 11  12 11 Oct 2016 (.0) 12 Sep 2016 (.8)



Description:

Mission details:


Ref.: #3(SD523,526,527,528), #7(JR716-717) - update: 28.03.17 Home