Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11881
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.2
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: 1992-093GF
Object number (NORAD): 22496
Object ID (CCSDS): 22496
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.021 minutes
Inclination: 71.2158 deg
SMA: 7279.673 km
Apoapsis: 967.373 km
Periapsis: 835.704 km
RAAN: 69.7835 deg
Eccentricy: 0.0090436
Argument of periapsis: 201.284 deg
Mean anomaly: 321.4872 deg
Mean motion: 13.97767454 rev/day
Mean motion (dot): 0.00000073 rev/day2
B* drag term: 0.000079747 1/REarth
Two-line elements (TLE)
Creation date: July 4, 2025, 6:39 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 4, 2025, 3:12 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22496U 92093GF 25185.13396947 .00000073 00000-0 79747-4 0 9997
TLE line 2: 2 22496 71.2158 69.7835 0090436 201.2840 321.4872 13.97767454654180
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.
