Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11881
Days in orbit
Revolutions
≈ 14.5
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: 99.004 minutes
Inclination: 71.1862 deg
SMA: 7089.191 km
Apoapsis: 731.122 km
Periapsis: 690.989 km
RAAN: 286.3976 deg
Eccentricy: 0.0028306
Argument of periapsis: 358.6986 deg
Mean anomaly: 1.4079 deg
Mean motion: 14.54480106 rev/day
Mean motion (dot): 0.00003355 rev/day2
B* drag term: 0.00079521 1/REarth
Two-line elements (TLE)
Creation date: July 4, 2025, 3:20 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 3, 2025, 5:03 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39718U 92093KJ 25184.71054508 .00003355 00000-0 79521-3 0 9994
TLE line 2: 2 39718 71.1862 286.3976 0028306 358.6986 1.4079 14.54480106588623
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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