Key statistics
Satellite SL-24 DEB at a glance.
Uptime
6656
Days in orbit
Revolutions
≈ 14.8
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
97.8
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: 2007-012D
Object number (NORAD): 31120
Object ID (CCSDS): 31120
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 97.064 minutes
Inclination: 97.7713 deg
SMA: 6996.274 km
Apoapsis: 623.084 km
Periapsis: 613.194 km
RAAN: 152.8304 deg
Eccentricy: 0.0007068
Argument of periapsis: 139.408 deg
Mean anomaly: 220.7662 deg
Mean motion: 14.8355109 rev/day
Mean motion (dot): 0.0000114 rev/day2
B* drag term: 0.0001447 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 10:26 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 8:48 p.m. UTC
TLE line 0: 0 SL-24 DEB
TLE line 1: 1 31120U 07012D 25187.86710739 .00001140 00000-0 14470-3 0 9996
TLE line 2: 2 31120 97.7713 152.8304 0007068 139.4080 220.7662 14.83551090981304
Live tracking on map
Real-time ground track for satellite SL-24 DEB.
Associated space launch
Rideshare mission with Egyptian and Saudi Arabian Earth observation satellites as well as 14 American cubesats
SL-24 DEB was lifted into orbit during the mission ‘Dnepr | EgyptSat 1 & Saudisat 3’, on board a Dnepr space rocket.
The launch took place on April 17, 2007, 6:46 a.m. from 109/95.
For more information about the launch, click the button.
Dnepr | EgyptSat 1 & Saudisat 3
Agency: N/A
Status: Launch Successful
Launch date: April 17, 2007, 6:46 a.m. UTC
Rocket: Dnepr
Launch pad: 109/95
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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