Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11791
Days in orbit
Revolutions
≈ 14.3
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: 1993-016CJ
Object number (NORAD): 39908
Object ID (CCSDS): 39908
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.95 minutes
Inclination: 71.002 deg
SMA: 7181.77 km
Apoapsis: 810.906 km
Periapsis: 796.364 km
RAAN: 164.5652 deg
Eccentricy: 0.0010124
Argument of periapsis: 203.0815 deg
Mean anomaly: 156.986 deg
Mean motion: 14.26446703 rev/day
Mean motion (dot): 0.00000557 rev/day2
B* drag term: 0.00025141 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 10:26 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 2:27 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39908U 93016CJ 25187.60264480 .00000557 00000-0 25141-3 0 9994
TLE line 2: 2 39908 71.0020 164.5652 0010124 203.0815 156.9860 14.26446703134197
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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