Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11875
Days in orbit
Revolutions
≈ 15.3
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: 1992-093AW
Object number (NORAD): 22357
Object ID (CCSDS): 22357
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 94.218 minutes
Inclination: 70.8482 deg
SMA: 6858.814 km
Apoapsis: 502.13 km
Periapsis: 459.228 km
RAAN: 43.0697 deg
Eccentricy: 0.0031275
Argument of periapsis: 131.1078 deg
Mean anomaly: 229.2811 deg
Mean motion: 15.28372437 rev/day
Mean motion (dot): 0.00021835 rev/day2
B* drag term: 0.00077905 1/REarth
Two-line elements (TLE)
Creation date: June 29, 2025, 2:41 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: June 28, 2025, 10:03 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22357U 92093AW 25179.91908641 .00021835 00000-0 77905-3 0 9994
TLE line 2: 2 22357 70.8482 43.0697 0031275 131.1078 229.2811 15.28372437716605
Live tracking on map
Real-time ground track for satellite 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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