Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11936
Days in orbit
Revolutions
≈ 14.3
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.8
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: 1992-093LN
Object number (NORAD): 39860
Object ID (CCSDS): 39860
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.583 minutes
Inclination: 70.7839 deg
SMA: 7164.368 km
Apoapsis: 807.961 km
Periapsis: 764.505 km
RAAN: 276.6005 deg
Eccentricy: 0.00303279
Argument of periapsis: 357.406 deg
Mean anomaly: 2.6908 deg
Mean motion: 14.3164692 rev/day
Mean motion (dot): 0.00001049 rev/day2
B* drag term: 0.00041077302 1/REarth
Two-line elements (TLE)
Creation date: Aug. 27, 2025, 2:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 26, 2025, 8:18 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39860U 92093LN 25238.84594326 .00001049 00000-0 41077-3 0 9996
TLE line 2: 2 39860 70.7839 276.6005 0030328 357.4060 2.6908 14.31646920584401
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
In-orbit conjunctions
A list of the most updated potential collisions computed for object 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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