Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11984
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: 103.261 minutes
Inclination: 70.7441 deg
SMA: 7290.949 km
Apoapsis: 1015.154 km
Periapsis: 810.475 km
RAAN: 254.2844 deg
Eccentricy: 0.01403653
Argument of periapsis: 355.7652 deg
Mean anomaly: 82.3114 deg
Mean motion: 13.94526046 rev/day
Mean motion (dot): 0.0000109 rev/day2
B* drag term: 0.00078462634 1/REarth
Two-line elements (TLE)
Creation date: Oct. 16, 2025, 2:37 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 15, 2025, 9:50 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22341U 92093AE 25288.91020934 .00001090 00000-0 78463-3 0 9999
TLE line 2: 2 22341 70.7441 254.2844 0140365 355.7652 82.3114 13.94526046663642
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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