Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12042
Days in orbit
Revolutions
≈ 14.6
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: 1992-093KJ
Object number (NORAD): 39718
Object ID (CCSDS): 39718
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.843 minutes
Inclination: 71.1851 deg
SMA: 7081.497 km
Apoapsis: 719.371 km
Periapsis: 687.353 km
RAAN: 285.2642 deg
Eccentricy: 0.00226068
Argument of periapsis: 92.6893 deg
Mean anomaly: 267.6841 deg
Mean motion: 14.56851068 rev/day
Mean motion (dot): 0.00013218 rev/day2
B* drag term: 0.002943276 1/REarth
Two-line elements (TLE)
Creation date: Dec. 13, 2025, 5:47 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 13, 2025, 6:05 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39718U 92093KJ 25347.25372674 .00013218 00000-0 29433-2 0 9996
TLE line 2: 2 39718 71.1851 285.2642 0022607 92.6893 267.6841 14.56851068612272
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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