Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11822
Days in orbit
Revolutions
≈ 14.2
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: 1992-093GU
Object number (NORAD): 22509
Object ID (CCSDS): 22509
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.115 minutes
Inclination: 71.1282 deg
SMA: 7189.601 km
Apoapsis: 886.858 km
Periapsis: 736.074 km
RAAN: 89.71 deg
Eccentricy: 0.0104862
Argument of periapsis: 38.7404 deg
Mean anomaly: 112.5468 deg
Mean motion: 14.24116721 rev/day
Mean motion (dot): 0.00004453 rev/day2
B* drag term: 0.0018454 1/REarth
Two-line elements (TLE)
Creation date: May 8, 2025, 3:01 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 7, 2025, 8:24 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22509U 92093GU 25127.35018209 .00004453 00000-0 18454-2 0 9996
TLE line 2: 2 22509 71.1282 89.7100 0104862 38.7404 112.5468 14.24116721657614
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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