Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11853
Days in orbit
Revolutions
≈ 13.9
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.0
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: 1993-016P
Object number (NORAD): 22605
Object ID (CCSDS): 22605
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.523 minutes
Inclination: 70.9968 deg
SMA: 7303.276 km
Apoapsis: 1018.235 km
Periapsis: 832.047 km
RAAN: 192.3223 deg
Eccentricy: 0.01274692
Argument of periapsis: 92.7413 deg
Mean anomaly: 25.8868 deg
Mean motion: 13.90997013 rev/day
Mean motion (dot): 0.00000347 rev/day2
B* drag term: 0.00029154721 1/REarth
Two-line elements (TLE)
Creation date: Sept. 6, 2025, 10:23 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 6, 2025, 4 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22605U 93016P 25249.16724363 .00000347 00000-0 29155-3 0 9997
TLE line 2: 2 22605 70.9968 192.3223 0127469 92.7413 25.8868 13.90997013644781
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
In-orbit conjunctions
A list of the most updated potential collisions computed for object 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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