Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12043
Days in orbit
Revolutions
≈ 13.9
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.8
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: 1992-093GM
Object number (NORAD): 22502
Object ID (CCSDS): 22502
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.625 minutes
Inclination: 70.8165 deg
SMA: 7308.099 km
Apoapsis: 1042.192 km
Periapsis: 817.736 km
RAAN: 349.4117 deg
Eccentricy: 0.01535664
Argument of periapsis: 198.6132 deg
Mean anomaly: 173.011 deg
Mean motion: 13.89620295 rev/day
Mean motion (dot): 0.00000286 rev/day2
B* drag term: 0.00024699106 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, 7:28 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22502U 92093GM 25348.31148375 .00000286 00000-0 24699-3 0 9997
TLE line 2: 2 22502 70.8165 349.4117 0153566 198.6132 173.0110 13.89620295668665
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 12’, on board a Zenit-2 space rocket.
The launch took place on Dec. 25, 1992, 5:56 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 12
Agency: N/A
Status: Launch Successful
Launch date: Dec. 25, 1992, 5:56 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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