Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11895
Days in orbit
Revolutions
≈ 13.9
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.0
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: 1993-016AB
Object number (NORAD): 22617
Object ID (CCSDS): 22617
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.442 minutes
Inclination: 70.9987 deg
SMA: 7299.491 km
Apoapsis: 1017.36 km
Periapsis: 825.352 km
RAAN: 230.9109 deg
Eccentricy: 0.01315216
Argument of periapsis: 143.5298 deg
Mean anomaly: 283.5009 deg
Mean motion: 13.92079161 rev/day
Mean motion (dot): 0.00000988 rev/day2
B* drag term: 0.00075185908 1/REarth
Two-line elements (TLE)
Creation date: Oct. 19, 2025, 2:20 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 18, 2025, 10:54 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22617U 93016AB 25291.95467053 .00000988 00000-0 75186-3 0 9990
TLE line 2: 2 22617 70.9987 230.9109 0131522 143.5298 283.5009 13.92079161646945
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 13’, on board a Zenit-2 space rocket.
The launch took place on March 26, 1993, 2:21 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 13
Agency: N/A
Status: Launch Successful
Launch date: March 26, 1993, 2:21 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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