Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11824
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: 103.292 minutes
Inclination: 71.1477 deg
SMA: 7292.423 km
Apoapsis: 1019.459 km
Periapsis: 809.117 km
RAAN: 37.8008 deg
Eccentricy: 0.0144219
Argument of periapsis: 288.5899 deg
Mean anomaly: 69.9595 deg
Mean motion: 13.94103371 rev/day
Mean motion (dot): 0.00000426 rev/day2
B* drag term: 0.00032596 1/REarth
Two-line elements (TLE)
Creation date: May 9, 2025, 2:46 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 8, 2025, 11:24 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39709U 92093JZ 25128.47524337 .00000426 00000-0 32596-3 0 9994
TLE line 2: 2 39709 71.1477 37.8008 0144219 288.5899 69.9595 13.94103371561796
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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