Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11882
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: 102.326 minutes
Inclination: 71.3362 deg
SMA: 7246.87 km
Apoapsis: 935.392 km
Periapsis: 802.078 km
RAAN: 122.1757 deg
Eccentricy: 0.009198
Argument of periapsis: 223.1844 deg
Mean anomaly: 136.2039 deg
Mean motion: 14.07268754 rev/day
Mean motion (dot): 0.00000823 rev/day2
B* drag term: 0.00049725 1/REarth
Two-line elements (TLE)
Creation date: July 3, 2025, 5:26 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 3, 2025, 1:43 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39850U 92093LC 25184.07218854 .00000823 00000-0 49725-3 0 9996
TLE line 2: 2 39850 71.3362 122.1757 0091980 223.1844 136.2039 14.07268754287202
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
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