Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11880
Days in orbit
Revolutions
≈ 14.2
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: 1992-093LK
Object number (NORAD): 39857
Object ID (CCSDS): 39857
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.069 minutes
Inclination: 70.9182 deg
SMA: 7187.393 km
Apoapsis: 850.781 km
Periapsis: 767.734 km
RAAN: 200.4506 deg
Eccentricy: 0.0057773
Argument of periapsis: 33.6322 deg
Mean anomaly: 326.845 deg
Mean motion: 14.24773077 rev/day
Mean motion (dot): 0.00001073 rev/day2
B* drag term: 0.00047314 1/REarth
Two-line elements (TLE)
Creation date: July 2, 2025, 5:47 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 2, 2025, 7:42 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39857U 92093LK 25183.32104577 .00001073 00000-0 47314-3 0 9996
TLE line 2: 2 39857 70.9182 200.4506 0057773 33.6322 326.8450 14.24773077573191
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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