Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11941
Days in orbit
Revolutions
≈ 13.9
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: 1992-093BL
Object number (NORAD): 22371
Object ID (CCSDS): 22371
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 103.317 minutes
Inclination: 71.1666 deg
SMA: 7293.576 km
Apoapsis: 997.385 km
Periapsis: 833.497 km
RAAN: 58.6238 deg
Eccentricy: 0.01123513
Argument of periapsis: 334.7249 deg
Mean anomaly: 198.6045 deg
Mean motion: 13.93772812 rev/day
Mean motion (dot): 0.00000268 rev/day2
B* drag term: 0.00022525726 1/REarth
Two-line elements (TLE)
Creation date: Sept. 3, 2025, 10:15 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 3, 2025, 5:45 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22371U 92093BL 25246.23997726 .00000268 00000-0 22526-3 0 9998
TLE line 2: 2 22371 71.1666 58.6238 0112351 334.7249 198.6045 13.93772812659399
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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