Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11882
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: 102.125 minutes
Inclination: 71.2753 deg
SMA: 7237.366 km
Apoapsis: 912.479 km
Periapsis: 805.982 km
RAAN: 273.3561 deg
Eccentricy: 0.0073574
Argument of periapsis: 227.8876 deg
Mean anomaly: 131.5978 deg
Mean motion: 14.10041816 rev/day
Mean motion (dot): 0.00000664 rev/day2
B* drag term: 0.00039154 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 10:36 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 3:05 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22394U 92093CK 25187.62913847 .00000664 00000-0 39154-3 0 9997
TLE line 2: 2 22394 71.2753 273.3561 0073574 227.8876 131.5978 14.10041816662712
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
...
Latest news about this satellite
There are no fresh news available about this satellite. Check back as we update our databases every day.
Newsletter sign-up
Weekly statistics, charts and insights to help you stay on top of the space industry.
