Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12042
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: 102.09 minutes
Inclination: 71.2775 deg
SMA: 7235.75 km
Apoapsis: 910.914 km
Periapsis: 804.316 km
RAAN: 304.712 deg
Eccentricy: 0.00736603
Argument of periapsis: 334.5982 deg
Mean anomaly: 25.1525 deg
Mean motion: 14.10514057 rev/day
Mean motion (dot): 0.00002355 rev/day2
B* drag term: 0.0013133414 1/REarth
Two-line elements (TLE)
Creation date: Dec. 14, 2025, 3:07 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 13, 2025, 1:56 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22394U 92093CK 25347.58093808 .00002355 00000-0 13133-2 0 9993
TLE line 2: 2 22394 71.2775 304.7120 0073660 334.5982 25.1525 14.10514057684987
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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