Key statistics
Satellite RUBIN 2 at a glance.
Uptime
8181
Days in orbit
Revolutions
≈ 14.8
Per day
Orbit
LEO
Low Earth Orbit
Inclination
64.6
Latest
Satellite identification and parameters
Extended collection of information and parameters for RUBIN 2.
Object identification
Identified? True
Debris? False
Object name: RUBIN 2
International designator: 2002-058A
Object number (NORAD): 27605
Object ID (CCSDS): 27605
Country: GERMANY (GER)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 97.388 minutes
Inclination: 64.5541 deg
SMA: 7011.833 km
Apoapsis: 672.405 km
Periapsis: 594.991 km
RAAN: 278.3362 deg
Eccentricy: 0.0055202
Argument of periapsis: 342.6281 deg
Mean anomaly: 17.2932 deg
Mean motion: 14.78616025 rev/day
Mean motion (dot): 0.00000627 rev/day2
B* drag term: 0.00010291 1/REarth
Two-line elements (TLE)
Creation date: May 14, 2025, 3:37 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 13, 2025, 7:07 p.m. UTC
TLE line 0: 0 RUBIN 2
TLE line 1: 1 27605U 02058A 25133.79668253 .00000627 00000-0 10291-3 0 9996
TLE line 2: 2 27605 64.5541 278.3362 0055202 342.6281 17.2932 14.78616025205515
Live tracking on map
Real-time ground track for satellite RUBIN 2.
Associated space launch
Technology satellite for OHB-System, Germany.
RUBIN 2 was lifted into orbit during the mission ‘Dnepr | AATiS-OSCAR-49’, on board a Dnepr space rocket.
The launch took place on Dec. 20, 2002, 5 p.m. from 109/95.
For more information about the launch, click the button.
Dnepr | AATiS-OSCAR-49
Agency: N/A
Status: Launch Successful
Launch date: Dec. 20, 2002, 5 p.m. UTC
Rocket: Dnepr
Launch pad: 109/95
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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