Key statistics
Satellite RUBIN 2 at a glance.
Uptime
8233
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: 97.383 minutes
Inclination: 64.5539 deg
SMA: 7011.599 km
Apoapsis: 676.441 km
Periapsis: 590.487 km
RAAN: 118.7603 deg
Eccentricy: 0.0061294
Argument of periapsis: 330.6988 deg
Mean anomaly: 29.0682 deg
Mean motion: 14.7868998 rev/day
Mean motion (dot): 0.00000576 rev/day2
B* drag term: 0.000095633 1/REarth
Two-line elements (TLE)
Creation date: July 4, 2025, 10:36 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 4, 2025, 5:43 p.m. UTC
TLE line 0: 0 RUBIN 2
TLE line 1: 1 27605U 02058A 25185.73854422 .00000576 00000-0 95633-4 0 9999
TLE line 2: 2 27605 64.5539 118.7603 0061294 330.6988 29.0682 14.78689980213259
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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