Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11937
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.3
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: 1992-093CK
Object number (NORAD): 22394
Object ID (CCSDS): 22394
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 102.118 minutes
Inclination: 71.2764 deg
SMA: 7237.044 km
Apoapsis: 910.291 km
Periapsis: 807.528 km
RAAN: 159.842 deg
Eccentricy: 0.00709978
Argument of periapsis: 141.3581 deg
Mean anomaly: 219.2653 deg
Mean motion: 14.10135743 rev/day
Mean motion (dot): 0.00001515 rev/day2
B* drag term: 0.00086116987 1/REarth
Two-line elements (TLE)
Creation date: Aug. 31, 2025, 2:26 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 30, 2025, 9:23 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22394U 92093CK 25242.89131841 .00001515 00000-0 86117-3 0 9991
TLE line 2: 2 22394 71.2764 159.8420 0070998 141.3581 219.2653 14.10135743670228
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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