Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11940
Days in orbit
Revolutions
≈ 14.5
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.0
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: 1992-093GC
Object number (NORAD): 22493
Object ID (CCSDS): 22493
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.138 minutes
Inclination: 71.0389 deg
SMA: 7095.578 km
Apoapsis: 787.264 km
Periapsis: 647.622 km
RAAN: 136.836 deg
Eccentricy: 0.00984005
Argument of periapsis: 283.6189 deg
Mean anomaly: 75.401 deg
Mean motion: 14.52516593 rev/day
Mean motion (dot): 0.00003664 rev/day2
B* drag term: 0.00085440339 1/REarth
Two-line elements (TLE)
Creation date: Sept. 3, 2025, 2:21 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 2, 2025, 6:20 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22493U 92093GC 25245.76412619 .00003664 00000-0 85440-3 0 9990
TLE line 2: 2 22493 71.0389 136.8360 0098400 283.6189 75.4010 14.52516593729269
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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