Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11854
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: 102.843 minutes
Inclination: 70.9824 deg
SMA: 7271.288 km
Apoapsis: 988.869 km
Periapsis: 797.438 km
RAAN: 217.7775 deg
Eccentricy: 0.01316353
Argument of periapsis: 144.2648 deg
Mean anomaly: 7.087 deg
Mean motion: 14.00185908 rev/day
Mean motion (dot): 0.00002156 rev/day2
B* drag term: 0.0013833642 1/REarth
Two-line elements (TLE)
Creation date: Sept. 5, 2025, 10:27 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 3, 2025, 9:06 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39872U 93016AW 25246.37952281 .00002156 00000-0 13834-2 0 9999
TLE line 2: 2 39872 70.9824 217.7775 0131635 144.2648 7.0870 14.00185908572681
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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