Key statistics
Satellite RUBIN 2 at a glance.
Uptime
8394
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: 97.358 minutes
Inclination: 64.5542 deg
SMA: 7010.362 km
Apoapsis: 684.834 km
Periapsis: 579.62 km
RAAN: 345.3722 deg
Eccentricy: 0.00750416
Argument of periapsis: 298.0337 deg
Mean anomaly: 61.3191 deg
Mean motion: 14.79081548 rev/day
Mean motion (dot): 0.00001726 rev/day2
B* drag term: 0.00024120066 1/REarth
Two-line elements (TLE)
Creation date: Dec. 12, 2025, 10:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 6:38 a.m. UTC
TLE line 0: 0 RUBIN 2
TLE line 1: 1 27605U 02058A 25346.27680689 .00001726 00000-0 24120-3 0 9999
TLE line 2: 2 27605 64.5542 345.3722 0075042 298.0337 61.3191 14.79081548236935
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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