Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11882
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: 1992-093U
Object number (NORAD): 22331
Object ID (CCSDS): 22331
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 102.497 minutes
Inclination: 70.9224 deg
SMA: 7254.931 km
Apoapsis: 930.753 km
Periapsis: 822.839 km
RAAN: 109.2539 deg
Eccentricy: 0.0074373
Argument of periapsis: 83.8869 deg
Mean anomaly: 67.5813 deg
Mean motion: 14.04924067 rev/day
Mean motion (dot): -0.00000011 rev/day2
B* drag term: 0.000021786 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 5:26 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22331U 92093U 25187.22674775 -.00000011 00000-0 21786-4 0 9998
TLE line 2: 2 22331 70.9224 109.2539 0074373 83.8869 67.5813 14.04924067666489
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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