Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11823
Days in orbit
Revolutions
≈ 14.0
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: 1992-093KQ
Object number (NORAD): 39724
Object ID (CCSDS): 39724
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.655 minutes
Inclination: 70.8519 deg
SMA: 7262.411 km
Apoapsis: 949.005 km
Periapsis: 819.547 km
RAAN: 31.6084 deg
Eccentricy: 0.0089129
Argument of periapsis: 178.0298 deg
Mean anomaly: 182.1187 deg
Mean motion: 14.02754053 rev/day
Mean motion (dot): 0.0000059 rev/day2
B* drag term: 0.00039783 1/REarth
Two-line elements (TLE)
Creation date: May 7, 2025, 3:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 6, 2025, 9:24 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39724U 92093KQ 25126.39188893 .00000590 00000-0 39783-3 0 9990
TLE line 2: 2 39724 70.8519 31.6084 0089129 178.0298 182.1187 14.02754053565187
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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