Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11881
Days in orbit
Revolutions
≈ 13.9
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.2
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: 1992-093KS
Object number (NORAD): 39726
Object ID (CCSDS): 39726
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.506 minutes
Inclination: 71.157 deg
SMA: 7302.481 km
Apoapsis: 1012.442 km
Periapsis: 836.249 km
RAAN: 254.5919 deg
Eccentricy: 0.0120639
Argument of periapsis: 149.4647 deg
Mean anomaly: 31.4983 deg
Mean motion: 13.91224217 rev/day
Mean motion (dot): 0.00000032 rev/day2
B* drag term: 0.00005644 1/REarth
Two-line elements (TLE)
Creation date: July 5, 2025, 4:36 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 4, 2025, 10:47 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39726U 92093KS 25185.94934853 .00000032 00000-0 56440-4 0 9994
TLE line 2: 2 39726 71.1570 254.5919 0120639 149.4647 31.4983 13.91224217569236
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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