Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11882
Days in orbit
Revolutions
≈ 14.1
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: 1992-093M
Object number (NORAD): 22297
Object ID (CCSDS): 22297
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.407 minutes
Inclination: 70.946 deg
SMA: 7250.7 km
Apoapsis: 943.594 km
Periapsis: 801.537 km
RAAN: 169.6477 deg
Eccentricy: 0.0097961
Argument of periapsis: 47.3605 deg
Mean anomaly: 313.5718 deg
Mean motion: 14.0615381 rev/day
Mean motion (dot): 0.0 rev/day2
B* drag term: 0.000026997 1/REarth
Two-line elements (TLE)
Creation date: July 5, 2025, 5:45 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 5, 2025, 8:59 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22297U 92093M 25186.37470997 .00000000 00000-0 26997-4 0 9990
TLE line 2: 2 22297 70.9460 169.6477 0097961 47.3605 313.5718 14.06153810664639
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
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