Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11991
Days in orbit
Revolutions
≈ 14.1
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: 1992-093AL
Object number (NORAD): 22347
Object ID (CCSDS): 22347
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.448 minutes
Inclination: 70.8376 deg
SMA: 7252.649 km
Apoapsis: 989.184 km
Periapsis: 759.843 km
RAAN: 217.0221 deg
Eccentricy: 0.0158108
Argument of periapsis: 10.369 deg
Mean anomaly: 68.0222 deg
Mean motion: 14.05587232 rev/day
Mean motion (dot): 0.00005714 rev/day2
B* drag term: 0.0031606331 1/REarth
Two-line elements (TLE)
Creation date: Oct. 23, 2025, 6:40 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 23, 2025, 2:15 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22347U 92093AL 25296.09400124 .00005714 00000-0 31606-2 0 9990
TLE line 2: 2 22347 70.8376 217.0221 0158108 10.3690 68.0222 14.05587232656800
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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