Key statistics
Satellite SL-16 DEB at a glance.
Uptime
10694
Days in orbit
Revolutions
≈ 13.7
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.0
Latest
Satellite identification and parameters
Extended collection of information and parameters for SL-16 DEB.
Object identification
Identified? True
Debris? True
Object name: SL-16 DEB
International designator: 1996-051D
Object number (NORAD): 24300
Object ID (CCSDS): 24300
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.748 minutes
Inclination: 71.0273 deg
SMA: 7360.788 km
Apoapsis: 1126.627 km
Periapsis: 838.679 km
RAAN: 114.466 deg
Eccentricy: 0.0195596
Argument of periapsis: 349.0893 deg
Mean anomaly: 36.4523 deg
Mean motion: 13.74726536 rev/day
Mean motion (dot): 0.0000015 rev/day2
B* drag term: 0.00017694877 1/REarth
Two-line elements (TLE)
Creation date: Dec. 14, 2025, 6:24 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 14, 2025, 7:53 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 24300U 96051D 25348.32858156 .00000150 00000-0 17695-3 0 9997
TLE line 2: 2 24300 71.0273 114.4660 0195596 349.0893 36.4523 13.74726536467884
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
Associated space launch
Second generation ELING satellite
SL-16 DEB was lifted into orbit during the mission ‘Zenit-2 | Tselina-2 18’, on board a Zenit-2 space rocket.
The launch took place on Sept. 4, 1996, 9:01 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 18
Agency: N/A
Status: Launch Successful
Launch date: Sept. 4, 1996, 9:01 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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