Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12001
Days in orbit
Revolutions
≈ 14.4
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.0
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: 1992-093KZ
Object number (NORAD): 39847
Object ID (CCSDS): 39847
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.878 minutes
Inclination: 71.0292 deg
SMA: 7130.848 km
Apoapsis: 790.707 km
Periapsis: 714.719 km
RAAN: 219.6751 deg
Eccentricy: 0.00532812
Argument of periapsis: 75.9953 deg
Mean anomaly: 284.71 deg
Mean motion: 14.41753344 rev/day
Mean motion (dot): 0.00001742 rev/day2
B* drag term: 0.00053957072 1/REarth
Two-line elements (TLE)
Creation date: Oct. 16, 2025, 2:37 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 13, 2025, 2:35 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39847U 92093KZ 25286.10788392 .00001742 00000-0 53957-3 0 9991
TLE line 2: 2 39847 71.0292 219.6751 0053281 75.9953 284.7100 14.41753344596011
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.
