Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11941
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.9
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: 1992-093AR
Object number (NORAD): 22352
Object ID (CCSDS): 22352
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 102.807 minutes
Inclination: 70.8901 deg
SMA: 7269.549 km
Apoapsis: 947.222 km
Periapsis: 835.606 km
RAAN: 108.1385 deg
Eccentricy: 0.00767701
Argument of periapsis: 196.6069 deg
Mean anomaly: 280.2955 deg
Mean motion: 14.00688508 rev/day
Mean motion (dot): 0.0000004 rev/day2
B* drag term: 0.000057009726 1/REarth
Two-line elements (TLE)
Creation date: Sept. 3, 2025, 10:15 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 3, 2025, 1:10 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22352U 92093AR 25246.04864319 .00000040 00000-0 57010-4 0 9992
TLE line 2: 2 22352 70.8901 108.1385 0076770 196.6069 280.2955 14.00688508668631
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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