Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11846
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: 100.945 minutes
Inclination: 71.0027 deg
SMA: 7181.52 km
Apoapsis: 808.962 km
Periapsis: 797.808 km
RAAN: 48.7337 deg
Eccentricy: 0.0007766
Argument of periapsis: 108.4853 deg
Mean anomaly: 251.712 deg
Mean motion: 14.26521173 rev/day
Mean motion (dot): 0.00000962 rev/day2
B* drag term: 0.00041906033 1/REarth
Two-line elements (TLE)
Creation date: Aug. 30, 2025, 3:38 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 29, 2025, 5:42 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39908U 93016CJ 25241.73812600 .00000962 00000-0 41906-3 0 9999
TLE line 2: 2 39908 71.0027 48.7337 0007766 108.4853 251.7120 14.26521173583854
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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