Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11942
Days in orbit
Revolutions
≈ 14.6
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: 1992-093KJ
Object number (NORAD): 39718
Object ID (CCSDS): 39718
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.966 minutes
Inclination: 71.1861 deg
SMA: 7087.341 km
Apoapsis: 729.832 km
Periapsis: 688.581 km
RAAN: 152.2707 deg
Eccentricy: 0.00291017
Argument of periapsis: 260.6886 deg
Mean anomaly: 99.0967 deg
Mean motion: 14.5504945 rev/day
Mean motion (dot): 0.00012617 rev/day2
B* drag term: 0.0029150603 1/REarth
Two-line elements (TLE)
Creation date: Sept. 2, 2025, 10:20 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 2, 2025, 3:40 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39718U 92093KJ 25245.15343804 .00012617 00000-0 29151-2 0 9994
TLE line 2: 2 39718 71.1861 152.2707 0029102 260.6886 99.0967 14.55049450597411
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 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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