Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11881
Days in orbit
Revolutions
≈ 14.5
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: 1992-093KJ
Object number (NORAD): 39718
Object ID (CCSDS): 39718
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.004 minutes
Inclination: 71.1862 deg
SMA: 7089.191 km
Apoapsis: 731.122 km
Periapsis: 690.989 km
RAAN: 286.3976 deg
Eccentricy: 0.0028306
Argument of periapsis: 358.6986 deg
Mean anomaly: 1.4079 deg
Mean motion: 14.54480106 rev/day
Mean motion (dot): 0.00003355 rev/day2
B* drag term: 0.00079521 1/REarth
Two-line elements (TLE)
Creation date: July 4, 2025, 3:20 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 3, 2025, 5:03 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39718U 92093KJ 25184.71054508 .00003355 00000-0 79521-3 0 9994
TLE line 2: 2 39718 71.1862 286.3976 0028306 358.6986 1.4079 14.54480106588623
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.