Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11882
Days in orbit
Revolutions
≈ 14.2
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.1
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: 1992-093GU
Object number (NORAD): 22509
Object ID (CCSDS): 22509
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.094 minutes
Inclination: 71.1293 deg
SMA: 7188.572 km
Apoapsis: 886.971 km
Periapsis: 733.902 km
RAAN: 322.522 deg
Eccentricy: 0.0106467
Argument of periapsis: 305.5966 deg
Mean anomaly: 84.2539 deg
Mean motion: 14.24422614 rev/day
Mean motion (dot): 0.00001456 rev/day2
B* drag term: 0.00061252 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, 8:58 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22509U 92093GU 25187.37423755 .00001456 00000-0 61252-3 0 9995
TLE line 2: 2 22509 71.1293 322.5220 0106467 305.5966 84.2539 14.24422614666163
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.
