Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12043
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: 99.308 minutes
Inclination: 71.1186 deg
SMA: 7103.659 km
Apoapsis: 787.216 km
Periapsis: 663.831 km
RAAN: 138.3369 deg
Eccentricy: 0.0086846
Argument of periapsis: 301.5883 deg
Mean anomaly: 239.4586 deg
Mean motion: 14.50038804 rev/day
Mean motion (dot): 0.00009269 rev/day2
B* drag term: 0.0022875839 1/REarth
Two-line elements (TLE)
Creation date: Dec. 14, 2025, 6:24 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 14, 2025, 4:33 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 44574U 92093LW 25348.18981376 .00009269 00000-0 22876-2 0 9995
TLE line 2: 2 44574 71.1186 138.3369 0086846 301.5883 239.4586 14.50038804627907
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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