Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11994
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: 1992-093ET
Object number (NORAD): 22454
Object ID (CCSDS): 22454
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.871 minutes
Inclination: 70.9159 deg
SMA: 7272.565 km
Apoapsis: 969.943 km
Periapsis: 818.918 km
RAAN: 165.9061 deg
Eccentricy: 0.01038319
Argument of periapsis: 154.934 deg
Mean anomaly: 205.6868 deg
Mean motion: 13.99817124 rev/day
Mean motion (dot): 0.00000341 rev/day2
B* drag term: 0.00025206984 1/REarth
Two-line elements (TLE)
Creation date: Oct. 27, 2025, 2:46 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 26, 2025, 9:16 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22454U 92093ET 25299.88617073 .00000341 00000-0 25207-3 0 9994
TLE line 2: 2 22454 70.9159 165.9061 0103832 154.9340 205.6868 13.99817124672321
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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