Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11884
Days in orbit
Revolutions
≈ 14.1
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: 1992-093LB
Object number (NORAD): 39849
Object ID (CCSDS): 39849
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.45 minutes
Inclination: 70.8642 deg
SMA: 7252.717 km
Apoapsis: 934.212 km
Periapsis: 814.952 km
RAAN: 236.698 deg
Eccentricy: 0.0082218
Argument of periapsis: 25.5697 deg
Mean anomaly: 334.9451 deg
Mean motion: 14.05567385 rev/day
Mean motion (dot): 0.00000303 rev/day2
B* drag term: 0.00020866 1/REarth
Two-line elements (TLE)
Creation date: June 27, 2025, 3:01 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: June 26, 2025, 7:42 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39849U 92093LB 25177.82132467 .00000303 00000-0 20866-3 0 9992
TLE line 2: 2 39849 70.8642 236.6980 0082218 25.5697 334.9451 14.05567385567169
Live tracking on map
Real-time ground track for satellite 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
...
Latest news about this satellite
There are no fresh news available about this satellite. Check back as we update our databases every day.
Newsletter sign-up
Weekly statistics, charts and insights to help you stay on top of the space industry.
