Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12042
Days in orbit
Revolutions
≈ 14.3
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: 1992-093BR
Object number (NORAD): 22376
Object ID (CCSDS): 22376
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.701 minutes
Inclination: 70.8889 deg
SMA: 7169.93 km
Apoapsis: 832.703 km
Periapsis: 750.887 km
RAAN: 69.7918 deg
Eccentricy: 0.00570553
Argument of periapsis: 321.9017 deg
Mean anomaly: 190.0273 deg
Mean motion: 14.29981358 rev/day
Mean motion (dot): 0.00003091 rev/day2
B* drag term: 0.0011955914 1/REarth
Two-line elements (TLE)
Creation date: Dec. 14, 2025, 3:07 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 13, 2025, 3:54 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22376U 92093BR 25347.66292861 .00003091 00000-0 11956-2 0 9991
TLE line 2: 2 22376 70.8889 69.7918 0057055 321.9017 190.0273 14.29981358699463
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.
