Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11881
Days in orbit
Revolutions
≈ 15.3
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.3
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: 1992-093HD
Object number (NORAD): 22543
Object ID (CCSDS): 22543
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 94.338 minutes
Inclination: 71.3364 deg
SMA: 6864.625 km
Apoapsis: 495.616 km
Periapsis: 477.364 km
RAAN: 191.7606 deg
Eccentricy: 0.0013294
Argument of periapsis: 351.2611 deg
Mean anomaly: 8.8338 deg
Mean motion: 15.26432184 rev/day
Mean motion (dot): 0.00200716 rev/day2
B* drag term: 0.0074733 1/REarth
Two-line elements (TLE)
Creation date: July 5, 2025, 5:45 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 5, 2025, 9:22 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22543U 92093HD 25186.39082368 .00200716 00000-0 74733-2 0 9992
TLE line 2: 2 22543 71.3364 191.7606 0013294 351.2611 8.8338 15.26432184674272
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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