Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11847
Days in orbit
Revolutions
≈ 14.5
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: 1993-016F
Object number (NORAD): 22578
Object ID (CCSDS): 22578
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 99.126 minutes
Inclination: 71.0621 deg
SMA: 7094.975 km
Apoapsis: 794.092 km
Periapsis: 639.588 km
RAAN: 69.9398 deg
Eccentricy: 0.01088827
Argument of periapsis: 335.2133 deg
Mean anomaly: 130.3738 deg
Mean motion: 14.52701804 rev/day
Mean motion (dot): 0.00000822 rev/day2
B* drag term: 0.00019897336 1/REarth
Two-line elements (TLE)
Creation date: Sept. 1, 2025, 2:20 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 31, 2025, 8:44 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22578U 93016F 25243.86435718 .00000822 00000-0 19897-3 0 9990
TLE line 2: 2 22578 71.0621 69.9398 0108883 335.2133 130.3738 14.52701804713283
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 13’, on board a Zenit-2 space rocket.
The launch took place on March 26, 1993, 2:21 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 13
Agency: N/A
Status: Launch Successful
Launch date: March 26, 1993, 2:21 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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