Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11990
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: 99.406 minutes
Inclination: 71.1189 deg
SMA: 7108.338 km
Apoapsis: 790.902 km
Periapsis: 669.503 km
RAAN: 257.2041 deg
Eccentricy: 0.00853924
Argument of periapsis: 26.556 deg
Mean anomaly: 124.3745 deg
Mean motion: 14.4860741 rev/day
Mean motion (dot): 0.00018784 rev/day2
B* drag term: 0.0047660943 1/REarth
Two-line elements (TLE)
Creation date: Oct. 21, 2025, 6:24 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 21, 2025, 8:25 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 44574U 92093LW 25294.35117205 .00018784 00000-0 47661-2 0 9997
TLE line 2: 2 44574 71.1189 257.2041 0085392 26.5560 124.3745 14.48607410620105
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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