Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11883
Days in orbit
Revolutions
≈ 14.1
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: 1992-093JH
Object number (NORAD): 23302
Object ID (CCSDS): 23302
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.933 minutes
Inclination: 71.137 deg
SMA: 7228.304 km
Apoapsis: 934.319 km
Periapsis: 766.018 km
RAAN: 150.7596 deg
Eccentricy: 0.0116418
Argument of periapsis: 118.4389 deg
Mean anomaly: 356.0851 deg
Mean motion: 14.12694228 rev/day
Mean motion (dot): 0.00001223 rev/day2
B* drag term: 0.00064126 1/REarth
Two-line elements (TLE)
Creation date: July 4, 2025, 6:39 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 4, 2025, 2:13 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23302U 92093JH 25185.59251356 .00001223 00000-0 64126-3 0 9990
TLE line 2: 2 23302 71.1370 150.7596 0116418 118.4389 356.0851 14.12694228605108
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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