Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11951
Days in orbit
Revolutions
≈ 13.9
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: 1993-016CH
Object number (NORAD): 39907
Object ID (CCSDS): 39907
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.626 minutes
Inclination: 70.9926 deg
SMA: 7308.13 km
Apoapsis: 1022.965 km
Periapsis: 837.025 km
RAAN: 113.0588 deg
Eccentricy: 0.01272145
Argument of periapsis: 76.9474 deg
Mean anomaly: 284.58 deg
Mean motion: 13.89611257 rev/day
Mean motion (dot): 0.00000582 rev/day2
B* drag term: 0.00047912373 1/REarth
Two-line elements (TLE)
Creation date: Dec. 13, 2025, 4:32 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 2:58 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39907U 93016CH 25346.62384418 .00000582 00000-0 47912-3 0 9994
TLE line 2: 2 39907 70.9926 113.0588 0127214 76.9474 284.5800 13.89611257585843
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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