Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11954
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: 100.925 minutes
Inclination: 71.0012 deg
SMA: 7180.596 km
Apoapsis: 810.687 km
Periapsis: 794.235 km
RAAN: 179.4368 deg
Eccentricy: 0.00114562
Argument of periapsis: 294.3442 deg
Mean anomaly: 65.649 deg
Mean motion: 14.26796412 rev/day
Mean motion (dot): 0.00000819 rev/day2
B* drag term: 0.00035764848 1/REarth
Two-line elements (TLE)
Creation date: Dec. 15, 2025, 4:20 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 14, 2025, 8:58 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39908U 93016CJ 25348.87391769 .00000819 00000-0 35765-3 0 9997
TLE line 2: 2 39908 71.0012 179.4368 0011456 294.3442 65.6490 14.26796412599134
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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