Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11792
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: 103.454 minutes
Inclination: 70.9996 deg
SMA: 7300.042 km
Apoapsis: 1020.152 km
Periapsis: 823.663 km
RAAN: 79.1574 deg
Eccentricy: 0.0134581
Argument of periapsis: 293.1182 deg
Mean anomaly: 86.1654 deg
Mean motion: 13.91921347 rev/day
Mean motion (dot): 0.00000391 rev/day2
B* drag term: 0.00031827 1/REarth
Two-line elements (TLE)
Creation date: July 8, 2025, 2:27 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 7, 2025, 11:15 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22617U 93016AB 25188.96879101 .00000391 00000-0 31827-3 0 9999
TLE line 2: 2 22617 70.9996 79.1574 0134581 293.1182 86.1654 13.91921347632619
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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