Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11944
Days in orbit
Revolutions
≈ 13.9
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: 1992-093ES
Object number (NORAD): 22453
Object ID (CCSDS): 22453
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.696 minutes
Inclination: 70.807 deg
SMA: 7311.42 km
Apoapsis: 1054.402 km
Periapsis: 812.168 km
RAAN: 353.1407 deg
Eccentricy: 0.01656546
Argument of periapsis: 133.3578 deg
Mean anomaly: 344.6068 deg
Mean motion: 13.886735 rev/day
Mean motion (dot): 0.00001128 rev/day2
B* drag term: 0.00087236543 1/REarth
Two-line elements (TLE)
Creation date: Sept. 6, 2025, 2:09 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 5, 2025, 5:11 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22453U 92093ES 25248.71617941 .00001128 00000-0 87237-3 0 9998
TLE line 2: 2 22453 70.8070 353.1407 0165655 133.3578 344.6068 13.88673500647639
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.
