Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11937
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.3
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: 1992-093LC
Object number (NORAD): 39850
Object ID (CCSDS): 39850
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.319 minutes
Inclination: 71.3384 deg
SMA: 7246.569 km
Apoapsis: 933.89 km
Periapsis: 802.977 km
RAAN: 14.9605 deg
Eccentricy: 0.00903282
Argument of periapsis: 140.7205 deg
Mean anomaly: 220.0516 deg
Mean motion: 14.07356612 rev/day
Mean motion (dot): 0.00000686 rev/day2
B* drag term: 0.0004181108 1/REarth
Two-line elements (TLE)
Creation date: Aug. 25, 2025, 2:12 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 24, 2025, 4:06 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39850U 92093LC 25236.67126808 .00000686 00000-0 41811-3 0 9992
TLE line 2: 2 39850 71.3384 14.9605 0090328 140.7205 220.0516 14.07356612294601
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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