Iridium-NEXT SV102-SV114

USA

Spacecraft nº:

US spacecraft nº:


Launch data:

Type Iridium-NEXT SV102 Iridium-NEXT SV103 Iridium-NEXT SV104 Iridium-NEXT SV105 Iridium-NEXT SV106 Iridium-NEXT SV108 Iridium-NEXT SV109 Iridium-NEXT SV111 Iridium-NEXT SV112 Iridium-NEXT SV114
NORAD ID 41920 41918 41922 41921 41917 41924 41919 41926 41925 41923
Designation 17003D 17003B 17003F 17003E 17003A 17003H 17003C 17003K 17003J 17003G
Launch date 14 Jan 2017 - 17:54 UT
Launch site Va, SLC4E
Launch vehicle Falcon-9 v1.2
Mission Communication
Polar LEO orbit:
Perigee / Apogee 608 x 621 km 610 x 622 km 610 x 621 605 x 619 617 x 626 607 x 622 608 x 621 609 x 622 604 x 621 610 x 617
Eccentricity 8,59E-04 9,30E-04 1,00E-03 1,00E-03 2,12E-04 1,00E-03 8,59E-04 1,07E-03 1,07E-03 1,00E-03
Inclination  86.7°  86.7°  86.7°  86.7°  86.7°  86.7°  86.7°  86.7°  86.7°  86.7°
Period 100.4 min 100.4 min 100.4 min 97.0 min 100.4 min 97.0 min 100.4 min 100.4 min 100.4 min 100.4 min
Decay  2  3 4 5 6 8 9 11; 12 14



Spacecraft data:

Prime manufacturer Thales Alenia Space (prime), Orbital (integration)
Platform ELiTeBus-1000
Operator Iridium Communications Inc.
Mass at launch  860 kg
Dry Mass 678 kg
Basic shape  
Dimension (m) 
Equipment 
Solar array 2 deployable solar arrays
Stabilization  
Propulsion 
DC power  50 W
Design lifetime  10 years (design), 15 years (planned)


Description:

Mission details:

External links:


Ref.: #7(JR734,735), #14, #226, #228 - update: 11.12.17 Home