Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11882
Days in orbit
Revolutions
≈ 14.6
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.1
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: 1992-093BF
Object number (NORAD): 22366
Object ID (CCSDS): 22366
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 98.55 minutes
Inclination: 71.108 deg
SMA: 7067.48 km
Apoapsis: 742.439 km
Periapsis: 636.252 km
RAAN: 79.3897 deg
Eccentricy: 0.0075124
Argument of periapsis: 173.6553 deg
Mean anomaly: 269.4433 deg
Mean motion: 14.61187127 rev/day
Mean motion (dot): 0.00008125 rev/day2
B* drag term: 0.0015936 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 10:46 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 10:08 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22366U 92093BF 25187.92272882 .00008125 00000-0 15936-2 0 9997
TLE line 2: 2 22366 71.1080 79.3897 0075124 173.6553 269.4433 14.61187127673724
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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