Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11993
Days in orbit
Revolutions
≈ 13.7
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.1
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: 1992-093H
Object number (NORAD): 22293
Object ID (CCSDS): 22293
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.755 minutes
Inclination: 71.0557 deg
SMA: 7361.116 km
Apoapsis: 1128.924 km
Periapsis: 837.037 km
RAAN: 189.5016 deg
Eccentricy: 0.01982629
Argument of periapsis: 228.7227 deg
Mean anomaly: 129.6656 deg
Mean motion: 13.74634648 rev/day
Mean motion (dot): 0.00000114 rev/day2
B* drag term: 0.00014400513 1/REarth
Two-line elements (TLE)
Creation date: Oct. 26, 2025, 2:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 25, 2025, 8:35 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22293U 92093H 25298.85827603 .00000114 00000-0 14401-3 0 9995
TLE line 2: 2 22293 71.0557 189.5016 0198263 228.7227 129.6656 13.74634648640409
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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