Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11944
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.2
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: 1992-093GF
Object number (NORAD): 22496
Object ID (CCSDS): 22496
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.02 minutes
Inclination: 71.2155 deg
SMA: 7279.607 km
Apoapsis: 965.156 km
Periapsis: 837.788 km
RAAN: 299.9591 deg
Eccentricy: 0.00874827
Argument of periapsis: 103.1129 deg
Mean anomaly: 269.8296 deg
Mean motion: 13.977866 rev/day
Mean motion (dot): 0.00000159 rev/day2
B* drag term: 0.00013883974 1/REarth
Two-line elements (TLE)
Creation date: Sept. 7, 2025, 3:09 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 6, 2025, 10:33 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22496U 92093GF 25249.43997072 .00000159 00000-0 13884-3 0 9991
TLE line 2: 2 22496 71.2155 299.9591 0087483 103.1129 269.8296 13.97786600663179
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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