Key statistics
Satellite SL-24 R/B at a glance.
Uptime
5558
Days in orbit
Revolutions
≈ 14.3
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
97.4
Latest
Satellite identification and parameters
Extended collection of information and parameters for SL-24 R/B.
Object identification
Identified? True
Debris? False
Object name: SL-24 R/B
International designator: 2010-030B
Object number (NORAD): 36606
Object ID (CCSDS): 36606
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 100.83 minutes
Inclination: 97.4173 deg
SMA: 7176.076 km
Apoapsis: 1100.704 km
Periapsis: 495.177 km
RAAN: 214.2828 deg
Eccentricy: 0.04219069
Argument of periapsis: 14.9763 deg
Mean anomaly: 346.3477 deg
Mean motion: 14.28144792 rev/day
Mean motion (dot): 0.00002287 rev/day2
B* drag term: 0.00035628531 1/REarth
Two-line elements (TLE)
Creation date: Sept. 8, 2025, 3:16 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 7, 2025, 8:54 p.m. UTC
TLE line 0: 0 SL-24 R/B
TLE line 1: 1 36606U 10030B 25250.87115708 .00002287 00000-0 35629-3 0 9993
TLE line 2: 2 36606 97.4173 214.2828 0421907 14.9763 346.3477 14.28144792790859
Live tracking on map
Real-time ground track for satellite SL-24 R/B.
In-orbit conjunctions
A list of the most updated potential collisions computed for object SL-24 R/B.
Associated space launch
SL-24 R/B was lifted into orbit during the mission ‘Dnepr 1 | TanDEM-X’, on board a Dnepr space rocket.
The launch took place on June 21, 2010, 2:14 a.m. from 109/95.
For more information about the launch, click the button.

Dnepr 1 | TanDEM-X
Agency: N/A
Status: Launch Successful
Launch date: June 21, 2010, 2:14 a.m. UTC
Rocket: Dnepr
Launch pad: 109/95
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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