Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11986
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: 100.836 minutes
Inclination: 71.3482 deg
SMA: 7176.378 km
Apoapsis: 887.352 km
Periapsis: 709.134 km
RAAN: 79.14 deg
Eccentricy: 0.01241696
Argument of periapsis: 244.5745 deg
Mean anomaly: 267.4087 deg
Mean motion: 14.28054636 rev/day
Mean motion (dot): 0.00004784 rev/day2
B* drag term: 0.0017895444 1/REarth
Two-line elements (TLE)
Creation date: Oct. 18, 2025, 2:17 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 17, 2025, 8:34 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22426U 92093DT 25290.85715418 .00004784 00000-0 17895-2 0 9991
TLE line 2: 2 22426 71.3482 79.1400 0124170 244.5745 267.4087 14.28054636688577
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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