Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11883
Days in orbit
Revolutions
≈ 13.8
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.3
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: 1992-093AA
Object number (NORAD): 22337
Object ID (CCSDS): 22337
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 104.008 minutes
Inclination: 71.2903 deg
SMA: 7326.052 km
Apoapsis: 1055.416 km
Periapsis: 840.417 km
RAAN: 278.291 deg
Eccentricy: 0.0146736
Argument of periapsis: 47.851 deg
Mean anomaly: 313.4956 deg
Mean motion: 13.84515379 rev/day
Mean motion (dot): -0.00000006 rev/day2
B* drag term: 0.000028806 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 10:46 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 4:52 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22337U 92093AA 25187.70283811 -.00000006 00000-0 28806-4 0 9998
TLE line 2: 2 22337 71.2903 278.2910 0146736 47.8510 313.4956 13.84515379642023
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.
