Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11989
Days in orbit
Revolutions
≈ 13.9
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.1
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: 1992-093JZ
Object number (NORAD): 39709
Object ID (CCSDS): 39709
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.276 minutes
Inclination: 71.1462 deg
SMA: 7291.67 km
Apoapsis: 1016.739 km
Periapsis: 810.331 km
RAAN: 64.2083 deg
Eccentricy: 0.0141537
Argument of periapsis: 41.0808 deg
Mean anomaly: 320.0858 deg
Mean motion: 13.94319363 rev/day
Mean motion (dot): 0.00000753 rev/day2
B* drag term: 0.00055116581 1/REarth
Two-line elements (TLE)
Creation date: Oct. 21, 2025, 6:24 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 21, 2025, 1:38 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39709U 92093JZ 25294.06817224 .00000753 00000-0 55117-3 0 9990
TLE line 2: 2 39709 71.1462 64.2083 0141537 41.0808 320.0858 13.94319363584876
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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