Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11822
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: 102.132 minutes
Inclination: 71.2764 deg
SMA: 7237.7 km
Apoapsis: 912.816 km
Periapsis: 806.314 km
RAAN: 36.1911 deg
Eccentricy: 0.0073574
Argument of periapsis: 318.6934 deg
Mean anomaly: 40.8636 deg
Mean motion: 14.09944121 rev/day
Mean motion (dot): 0.00000624 rev/day2
B* drag term: 0.00037019 1/REarth
Two-line elements (TLE)
Creation date: May 8, 2025, 3:01 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 7, 2025, 7:45 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22394U 92093CK 25127.82350568 .00000624 00000-0 37019-3 0 9992
TLE line 2: 2 22394 71.2764 36.1911 0073574 318.6934 40.8636 14.09944121654007
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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