Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11937
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: 103.158 minutes
Inclination: 71.2347 deg
SMA: 7286.102 km
Apoapsis: 990.467 km
Periapsis: 825.466 km
RAAN: 91.3091 deg
Eccentricy: 0.01132297
Argument of periapsis: 123.4516 deg
Mean anomaly: 254.7002 deg
Mean motion: 13.95918 rev/day
Mean motion (dot): 0.0000027 rev/day2
B* drag term: 0.0002169854 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, 8:11 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22430U 92093DX 25241.84156573 .00000270 00000-0 21699-3 0 9996
TLE line 2: 2 22430 71.2347 91.3091 0113230 123.4516 254.7002 13.95918000659817
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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