Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11942
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: 1992-093JT
Object number (NORAD): 39302
Object ID (CCSDS): 39302
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.802 minutes
Inclination: 70.9784 deg
SMA: 7174.757 km
Apoapsis: 881.777 km
Periapsis: 711.467 km
RAAN: 255.4077 deg
Eccentricy: 0.01186873
Argument of periapsis: 39.0634 deg
Mean anomaly: 339.0536 deg
Mean motion: 14.28538631 rev/day
Mean motion (dot): 0.00005654 rev/day2
B* drag term: 0.0021066346 1/REarth
Two-line elements (TLE)
Creation date: Sept. 1, 2025, 2:20 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 31, 2025, 7:36 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39302U 92093JT 25243.31683497 .00005654 00000-0 21066-2 0 9994
TLE line 2: 2 39302 70.9784 255.4077 0118687 39.0634 339.0536 14.28538631616823
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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