Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11988
Days in orbit
Revolutions
≈ 13.9
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: 1992-093KS
Object number (NORAD): 39726
Object ID (CCSDS): 39726
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.503 minutes
Inclination: 71.1594 deg
SMA: 7302.35 km
Apoapsis: 1013.429 km
Periapsis: 835.0 km
RAAN: 43.5152 deg
Eccentricy: 0.01221723
Argument of periapsis: 350.9082 deg
Mean anomaly: 40.0661 deg
Mean motion: 13.91261666 rev/day
Mean motion (dot): 0.00000123 rev/day2
B* drag term: 0.00012446827 1/REarth
Two-line elements (TLE)
Creation date: Oct. 18, 2025, 10:30 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 18, 2025, 7:46 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39726U 92093KS 25291.32425299 .00000123 00000-0 12447-3 0 9992
TLE line 2: 2 39726 71.1594 43.5152 0122172 350.9082 40.0661 13.91261666583899
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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