Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11991
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.9
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: 1992-093KQ
Object number (NORAD): 39724
Object ID (CCSDS): 39724
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.642 minutes
Inclination: 70.8512 deg
SMA: 7261.788 km
Apoapsis: 949.753 km
Periapsis: 817.552 km
RAAN: 43.9034 deg
Eccentricy: 0.00910254
Argument of periapsis: 291.2638 deg
Mean anomaly: 67.8775 deg
Mean motion: 14.02934651 rev/day
Mean motion (dot): 0.0000076 rev/day2
B* drag term: 0.0005024104 1/REarth
Two-line elements (TLE)
Creation date: Oct. 21, 2025, 6:24 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 21, 2025, 12:42 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39724U 92093KQ 25294.02940731 .00000760 00000-0 50241-3 0 9994
TLE line 2: 2 39724 70.8512 43.9034 0091025 291.2638 67.8775 14.02934651588692
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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