Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11951
Days in orbit
Revolutions
≈ 13.8
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: 1993-016V
Object number (NORAD): 22611
Object ID (CCSDS): 22611
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.448 minutes
Inclination: 70.9894 deg
SMA: 7346.72 km
Apoapsis: 1094.144 km
Periapsis: 843.025 km
RAAN: 114.675 deg
Eccentricy: 0.01709059
Argument of periapsis: 338.6264 deg
Mean anomaly: 138.7561 deg
Mean motion: 13.78677094 rev/day
Mean motion (dot): 0.00000287 rev/day2
B* drag term: 0.00029229147 1/REarth
Two-line elements (TLE)
Creation date: Dec. 12, 2025, 10:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 1:03 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22611U 93016V 25346.04405416 .00000287 00000-0 29229-3 0 9999
TLE line 2: 2 22611 70.9894 114.6750 0170906 338.6264 138.7561 13.78677094643646
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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