Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11882
Days in orbit
Revolutions
≈ 13.9
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.9
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: 1992-093BJ
Object number (NORAD): 22369
Object ID (CCSDS): 22369
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 103.269 minutes
Inclination: 70.8863 deg
SMA: 7291.334 km
Apoapsis: 985.036 km
Periapsis: 841.362 km
RAAN: 113.2849 deg
Eccentricy: 0.0098524
Argument of periapsis: 123.7461 deg
Mean anomaly: 237.3086 deg
Mean motion: 13.94415812 rev/day
Mean motion (dot): -0.00000026 rev/day2
B* drag term: 0.000013717 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 4:31 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22369U 92093BJ 25187.18865007 -.00000026 00000-0 13717-4 0 9995
TLE line 2: 2 22369 70.8863 113.2849 0098524 123.7461 237.3086 13.94415812653658
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.
