Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11994
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.8
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: 1992-093KB
Object number (NORAD): 39711
Object ID (CCSDS): 39711
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.656 minutes
Inclination: 70.8377 deg
SMA: 7262.467 km
Apoapsis: 953.975 km
Periapsis: 814.688 km
RAAN: 27.7288 deg
Eccentricy: 0.00958955
Argument of periapsis: 287.5655 deg
Mean anomaly: 71.5001 deg
Mean motion: 14.02737925 rev/day
Mean motion (dot): 0.000008 rev/day2
B* drag term: 0.00052668615 1/REarth
Two-line elements (TLE)
Creation date: Oct. 27, 2025, 2:46 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 26, 2025, 12:07 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39711U 92093KB 25299.50543482 .00000800 00000-0 52669-3 0 9991
TLE line 2: 2 39711 70.8377 27.7288 0095895 287.5655 71.5001 14.02737925589379
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.
