Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11942
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: 101.076 minutes
Inclination: 71.1285 deg
SMA: 7187.74 km
Apoapsis: 886.292 km
Periapsis: 732.918 km
RAAN: 195.496 deg
Eccentricy: 0.01066915
Argument of periapsis: 212.7512 deg
Mean anomaly: 305.3719 deg
Mean motion: 14.24669867 rev/day
Mean motion (dot): 0.0000349 rev/day2
B* drag term: 0.0014324743 1/REarth
Two-line elements (TLE)
Creation date: Sept. 4, 2025, 10:13 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 4, 2025, 7:07 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22509U 92093GU 25247.29685992 .00003490 00000-0 14325-2 0 9994
TLE line 2: 2 22509 71.1285 195.4960 0106692 212.7512 305.3719 14.24669867674695
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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