Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11985
Days in orbit
Revolutions
≈ 14.0
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: 1992-093AY
Object number (NORAD): 22359
Object ID (CCSDS): 22359
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.119 minutes
Inclination: 70.7385 deg
SMA: 7284.267 km
Apoapsis: 1020.54 km
Periapsis: 791.724 km
RAAN: 88.276 deg
Eccentricy: 0.01570623
Argument of periapsis: 114.989 deg
Mean anomaly: 356.9525 deg
Mean motion: 13.96445457 rev/day
Mean motion (dot): 0.00002808 rev/day2
B* drag term: 0.0018617479 1/REarth
Two-line elements (TLE)
Creation date: Oct. 18, 2025, 2:17 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 17, 2025, 8:36 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22359U 92093AY 25290.85840743 .00002808 00000-0 18617-2 0 9994
TLE line 2: 2 22359 70.7385 88.2760 0157062 114.9890 356.9525 13.96445457657222
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
In-orbit conjunctions
A list of the most updated potential collisions computed for object 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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