Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12042
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.1
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: 1992-093JH
Object number (NORAD): 23302
Object ID (CCSDS): 23302
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.891 minutes
Inclination: 71.1304 deg
SMA: 7226.323 km
Apoapsis: 932.022 km
Periapsis: 764.355 km
RAAN: 184.8227 deg
Eccentricy: 0.01160112
Argument of periapsis: 237.6325 deg
Mean anomaly: 301.3149 deg
Mean motion: 14.13275045 rev/day
Mean motion (dot): 0.00002913 rev/day2
B* drag term: 0.0014800275 1/REarth
Two-line elements (TLE)
Creation date: Dec. 8, 2025, 6:20 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 8, 2025, 8:21 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23302U 92093JH 25342.34799404 .00002913 00000-0 14800-2 0 9999
TLE line 2: 2 23302 71.1304 184.8227 0116011 237.6325 301.3149 14.13275045627242
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
...
Latest news about this satellite
There are no fresh news available about this satellite. Check back as we update our databases every day.
Newsletter sign-up
Weekly statistics, charts and insights to help you stay on top of the space industry.
