Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11905
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: 1993-016CD
Object number (NORAD): 39903
Object ID (CCSDS): 39903
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.778 minutes
Inclination: 70.9895 deg
SMA: 7315.249 km
Apoapsis: 1035.66 km
Periapsis: 838.569 km
RAAN: 241.4432 deg
Eccentricy: 0.01347128
Argument of periapsis: 173.5479 deg
Mean anomaly: 4.2526 deg
Mean motion: 13.87583285 rev/day
Mean motion (dot): 0.0000032 rev/day2
B* drag term: 0.00028631111 1/REarth
Two-line elements (TLE)
Creation date: Oct. 26, 2025, 2:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 25, 2025, 1:59 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39903U 93016CD 25298.58332016 .00000320 00000-0 28631-3 0 9995
TLE line 2: 2 39903 70.9895 241.4432 0134713 173.5479 4.2526 13.87583285577861
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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