Key statistics
Satellite RUBIN 2 at a glance.
Uptime
8295
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: 97.378 minutes
Inclination: 64.5535 deg
SMA: 7011.317 km
Apoapsis: 680.615 km
Periapsis: 585.749 km
RAAN: 289.869 deg
Eccentricy: 0.00676521
Argument of periapsis: 317.5704 deg
Mean anomaly: 42.0181 deg
Mean motion: 14.78779293 rev/day
Mean motion (dot): 0.00001148 rev/day2
B* drag term: 0.00016956668 1/REarth
Two-line elements (TLE)
Creation date: Sept. 4, 2025, 10:13 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 4, 2025, 5:07 a.m. UTC
TLE line 0: 0 RUBIN 2
TLE line 1: 1 27605U 02058A 25247.21338358 .00001148 00000-0 16957-3 0 9993
TLE line 2: 2 27605 64.5535 289.8690 0067652 317.5704 42.0181 14.78779293222284
Live tracking on map
Real-time ground track for satellite RUBIN 2.
In-orbit conjunctions
A list of the most updated potential collisions computed for object 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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