Key statistics
Satellite SL-24 R/B at a glance.
Uptime
5495
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: 100.84 minutes
Inclination: 97.4088 deg
SMA: 7176.557 km
Apoapsis: 1100.828 km
Periapsis: 496.016 km
RAAN: 160.5694 deg
Eccentricy: 0.042138
Argument of periapsis: 205.6124 deg
Mean anomaly: 152.3645 deg
Mean motion: 14.28001118 rev/day
Mean motion (dot): 0.00000262 rev/day2
B* drag term: 0.000048498 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 10:56 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 9:07 p.m. UTC
TLE line 0: 0 SL-24 R/B
TLE line 1: 1 36606U 10030B 25187.88018441 .00000262 00000-0 48498-4 0 9999
TLE line 2: 2 36606 97.4088 160.5694 0421380 205.6124 152.3645 14.28001118781882
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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