Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11905
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: 102.83 minutes
Inclination: 70.9829 deg
SMA: 7270.638 km
Apoapsis: 989.039 km
Periapsis: 795.968 km
RAAN: 114.9374 deg
Eccentricy: 0.0132774
Argument of periapsis: 68.2329 deg
Mean anomaly: 325.3538 deg
Mean motion: 14.00373671 rev/day
Mean motion (dot): 0.00001725 rev/day2
B* drag term: 0.0011072 1/REarth
Two-line elements (TLE)
Creation date: Oct. 23, 2025, 10:06 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 23, 2025, 12:06 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39872U 93016AW 25296.50416925 .00001725 00000-0 11072-2 0 9992
TLE line 2: 2 39872 70.9829 114.9374 0132774 68.2329 325.3538 14.00373671579708
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
In-orbit conjunctions
A list of the most updated potential collisions computed for object 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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