Key statistics
Satellite SL-24 DEB at a glance.
Uptime
5824
Days in orbit
Revolutions
≈ 14.8
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
97.6
Latest
Satellite identification and parameters
Extended collection of information and parameters for SL-24 DEB.
Object identification
Identified? True
Debris? True
Object name: SL-24 DEB
International designator: 2009-041J
Object number (NORAD): 35689
Object ID (CCSDS): 35689
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 97.081 minutes
Inclination: 97.6209 deg
SMA: 6997.055 km
Apoapsis: 632.243 km
Periapsis: 605.597 km
RAAN: 9.9225 deg
Eccentricy: 0.0019041
Argument of periapsis: 319.8459 deg
Mean anomaly: 40.1348 deg
Mean motion: 14.83302814 rev/day
Mean motion (dot): 0.00001347 rev/day2
B* drag term: 0.00017034 1/REarth
Two-line elements (TLE)
Creation date: July 9, 2025, 2:22 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 8, 2025, 6:21 p.m. UTC
TLE line 0: 0 SL-24 DEB
TLE line 1: 1 35689U 09041J 25189.76460893 .00001347 00000-0 17034-3 0 9996
TLE line 2: 2 35689 97.6209 9.9225 0019041 319.8459 40.1348 14.83302814858147
Live tracking on map
Real-time ground track for satellite SL-24 DEB.
Associated space launch
Emirati Earth observation satellite. Launched with 5 secondary payloads.
SL-24 DEB was lifted into orbit during the mission ‘Dnepr | DubaiSat 1’, on board a Dnepr space rocket.
The launch took place on July 29, 2009, 6:46 p.m. from 109/95.
For more information about the launch, click the button.
Dnepr | DubaiSat 1
Agency: N/A
Status: Launch Successful
Launch date: July 29, 2009, 6:46 p.m. UTC
Rocket: Dnepr
Launch pad: 109/95
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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