Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11880
Days in orbit
Revolutions
≈ 14.3
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: 1992-093KF
Object number (NORAD): 39715
Object ID (CCSDS): 39715
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.561 minutes
Inclination: 71.0102 deg
SMA: 7163.322 km
Apoapsis: 789.496 km
Periapsis: 780.879 km
RAAN: 191.2098 deg
Eccentricy: 0.0006015
Argument of periapsis: 249.4254 deg
Mean anomaly: 110.6233 deg
Mean motion: 14.31960444 rev/day
Mean motion (dot): 0.00000723 rev/day2
B* drag term: 0.00028783 1/REarth
Two-line elements (TLE)
Creation date: July 4, 2025, 6:39 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 4, 2025, 9:19 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39715U 92093KF 25185.38852266 .00000723 00000-0 28783-3 0 9992
TLE line 2: 2 39715 71.0102 191.2098 0006015 249.4254 110.6233 14.31960444584717
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 12’, on board a Zenit-2 space rocket.
The launch took place on Dec. 25, 1992, 5:56 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 12
Agency: N/A
Status: Launch Successful
Launch date: Dec. 25, 1992, 5:56 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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