Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11991
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.2
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: 1992-093DX
Object number (NORAD): 22430
Object ID (CCSDS): 22430
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.155 minutes
Inclination: 71.2376 deg
SMA: 7285.962 km
Apoapsis: 990.379 km
Periapsis: 825.275 km
RAAN: 341.3343 deg
Eccentricy: 0.0113303
Argument of periapsis: 39.2429 deg
Mean anomaly: 78.1732 deg
Mean motion: 13.95958206 rev/day
Mean motion (dot): 0.00000281 rev/day2
B* drag term: 0.00022418 1/REarth
Two-line elements (TLE)
Creation date: Oct. 23, 2025, 10:16 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 23, 2025, 12:52 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22430U 92093DX 25296.53635367 .00000281 00000-0 22418-3 0 9997
TLE line 2: 2 22430 71.2376 341.3343 0113303 39.2429 78.1732 13.95958206667443
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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