Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11936
Days in orbit
Revolutions
≈ 13.9
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.7
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: 1992-093AE
Object number (NORAD): 22341
Object ID (CCSDS): 22341
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.266 minutes
Inclination: 70.748 deg
SMA: 7291.18 km
Apoapsis: 1013.818 km
Periapsis: 812.272 km
RAAN: 351.3437 deg
Eccentricy: 0.01382121
Argument of periapsis: 63.7642 deg
Mean anomaly: 56.698 deg
Mean motion: 13.94459802 rev/day
Mean motion (dot): 0.00000281 rev/day2
B* drag term: 0.00022645005 1/REarth
Two-line elements (TLE)
Creation date: Aug. 30, 2025, 3:38 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 29, 2025, 5:15 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22341U 92093AE 25241.71939897 .00000281 00000-0 22645-3 0 9995
TLE line 2: 2 22341 70.7480 351.3437 0138212 63.7642 56.6980 13.94459802657064
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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