Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11881
Days in orbit
Revolutions
≈ 14.5
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: 1992-093LW
Object number (NORAD): 44574
Object ID (CCSDS): 44574
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.539 minutes
Inclination: 71.1197 deg
SMA: 7114.702 km
Apoapsis: 801.171 km
Periapsis: 671.962 km
RAAN: 134.9443 deg
Eccentricy: 0.0090804
Argument of periapsis: 205.7406 deg
Mean anomaly: 313.0529 deg
Mean motion: 14.46664152 rev/day
Mean motion (dot): 0.00004619 rev/day2
B* drag term: 0.0012277 1/REarth
Two-line elements (TLE)
Creation date: July 5, 2025, 5:45 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 5, 2025, 8:02 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 44574U 92093LW 25186.33540787 .00004619 00000-0 12277-2 0 9997
TLE line 2: 2 44574 71.1197 134.9443 0090804 205.7406 313.0529 14.46664152604478
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
...
Latest news about this satellite
There are no fresh news available about this satellite. Check back as we update our databases every day.
Newsletter sign-up
Weekly statistics, charts and insights to help you stay on top of the space industry.
