Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11937
Days in orbit
Revolutions
≈ 14.3
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.3
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: 1992-093DT
Object number (NORAD): 22426
Object ID (CCSDS): 22426
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.856 minutes
Inclination: 71.3496 deg
SMA: 7177.289 km
Apoapsis: 888.725 km
Periapsis: 709.583 km
RAAN: 180.1716 deg
Eccentricy: 0.01247973
Argument of periapsis: 320.7065 deg
Mean anomaly: 103.9079 deg
Mean motion: 14.27782677 rev/day
Mean motion (dot): 0.00004234 rev/day2
B* drag term: 0.0015934076 1/REarth
Two-line elements (TLE)
Creation date: Aug. 31, 2025, 2:26 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 30, 2025, 10:09 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22426U 92093DT 25242.92293351 .00004234 00000-0 15934-2 0 9995
TLE line 2: 2 22426 71.3496 180.1716 0124797 320.7065 103.9079 14.27782677681730
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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