Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11791
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: 104.455 minutes
Inclination: 70.9904 deg
SMA: 7347.039 km
Apoapsis: 1094.369 km
Periapsis: 843.439 km
RAAN: 68.0654 deg
Eccentricy: 0.017077
Argument of periapsis: 206.2844 deg
Mean anomaly: 178.7793 deg
Mean motion: 13.78587186 rev/day
Mean motion (dot): 0.00000104 rev/day2
B* drag term: 0.00013044 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 3:12 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22611U 93016V 25187.63380735 .00000104 00000-0 13044-3 0 9999
TLE line 2: 2 22611 70.9904 68.0654 0170770 206.2844 178.7793 13.78587186621814
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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