Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11826
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: 101.946 minutes
Inclination: 71.1328 deg
SMA: 7228.942 km
Apoapsis: 937.55 km
Periapsis: 764.064 km
RAAN: 267.0409 deg
Eccentricy: 0.0119994
Argument of periapsis: 203.7527 deg
Mean anomaly: 173.5405 deg
Mean motion: 14.1250706 rev/day
Mean motion (dot): 0.0000252 rev/day2
B* drag term: 0.0012964 1/REarth
Two-line elements (TLE)
Creation date: May 10, 2025, 5:27 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 9, 2025, 3:09 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23302U 92093JH 25129.63178183 .00002520 00000-0 12964-2 0 9992
TLE line 2: 2 23302 71.1328 267.0409 0119994 203.7527 173.5405 14.12507060597205
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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