Key statistics
Satellite RUBIN 2 at a glance.
Uptime
8343
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: 97.368 minutes
Inclination: 64.5522 deg
SMA: 7010.848 km
Apoapsis: 682.845 km
Periapsis: 582.58 km
RAAN: 143.5559 deg
Eccentricy: 0.0071507
Argument of periapsis: 307.9772 deg
Mean anomaly: 51.4886 deg
Mean motion: 14.78927704 rev/day
Mean motion (dot): 0.00001099 rev/day2
B* drag term: 0.00016197 1/REarth
Two-line elements (TLE)
Creation date: Oct. 22, 2025, 12:16 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 21, 2025, 7:41 p.m. UTC
TLE line 0: 0 RUBIN 2
TLE line 1: 1 27605U 02058A 25294.82040513 .00001099 00000-0 16197-3 0 9996
TLE line 2: 2 27605 64.5522 143.5559 0071507 307.9772 51.4886 14.78927704229322
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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