Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11790
Days in orbit
Revolutions
≈ 14.0
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: 1993-016AW
Object number (NORAD): 39872
Object ID (CCSDS): 39872
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.857 minutes
Inclination: 70.9925 deg
SMA: 7271.943 km
Apoapsis: 991.554 km
Periapsis: 796.062 km
RAAN: 345.2646 deg
Eccentricy: 0.0134415
Argument of periapsis: 235.528 deg
Mean anomaly: 300.3581 deg
Mean motion: 13.99996835 rev/day
Mean motion (dot): 0.00000943 rev/day2
B* drag term: 0.00062178 1/REarth
Two-line elements (TLE)
Creation date: July 3, 2025, 5:26 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 3, 2025, 5:27 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39872U 93016AW 25184.22722153 .00000943 00000-0 62178-3 0 9995
TLE line 2: 2 39872 70.9925 345.2646 0134415 235.5280 300.3581 13.99996835563989
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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