Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11944
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: 99.473 minutes
Inclination: 71.1228 deg
SMA: 7111.545 km
Apoapsis: 794.882 km
Periapsis: 671.937 km
RAAN: 355.5329 deg
Eccentricy: 0.00864403
Argument of periapsis: 101.2056 deg
Mean anomaly: 17.3743 deg
Mean motion: 14.47627625 rev/day
Mean motion (dot): 0.00012275 rev/day2
B* drag term: 0.0031843283 1/REarth
Two-line elements (TLE)
Creation date: Sept. 7, 2025, 3:09 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 6, 2025, 5:14 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 44574U 92093LW 25249.71854039 .00012275 00000-0 31843-2 0 9994
TLE line 2: 2 44574 71.1228 355.5329 0086440 101.2056 17.3743 14.47627625613645
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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