Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11989
Days in orbit
Revolutions
≈ 14.3
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: 1992-093JT
Object number (NORAD): 39302
Object ID (CCSDS): 39302
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.738 minutes
Inclination: 70.9827 deg
SMA: 7171.688 km
Apoapsis: 879.661 km
Periapsis: 707.445 km
RAAN: 150.1117 deg
Eccentricy: 0.01200664
Argument of periapsis: 325.9358 deg
Mean anomaly: 151.5219 deg
Mean motion: 14.29455686 rev/day
Mean motion (dot): 0.00010445 rev/day2
B* drag term: 0.0037959889 1/REarth
Two-line elements (TLE)
Creation date: Oct. 19, 2025, 10:30 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 19, 2025, 6:25 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39302U 92093JT 25292.26793146 .00010445 00000-0 37960-2 0 9999
TLE line 2: 2 39302 70.9827 150.1117 0120066 325.9358 151.5219 14.29455686623812
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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