Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11880
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.8
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: 102.651 minutes
Inclination: 70.8484 deg
SMA: 7262.221 km
Apoapsis: 947.151 km
Periapsis: 821.021 km
RAAN: 270.9294 deg
Eccentricy: 0.008684
Argument of periapsis: 91.5836 deg
Mean anomaly: 269.5228 deg
Mean motion: 14.02809134 rev/day
Mean motion (dot): 0.00000247 rev/day2
B* drag term: 0.00018369 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, 1:53 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39724U 92093KQ 25184.57901366 .00000247 00000-0 18369-3 0 9998
TLE line 2: 2 39724 70.8484 270.9294 0086840 91.5836 269.5228 14.02809134573347
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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