Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11849
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: 1993-016AB
Object number (NORAD): 22617
Object ID (CCSDS): 22617
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.449 minutes
Inclination: 71.0012 deg
SMA: 7299.787 km
Apoapsis: 1019.535 km
Periapsis: 823.77 km
RAAN: 324.039 deg
Eccentricy: 0.01340895
Argument of periapsis: 210.9086 deg
Mean anomaly: 267.2921 deg
Mean motion: 13.91994344 rev/day
Mean motion (dot): 0.000013 rev/day2
B* drag term: 0.00097850453 1/REarth
Two-line elements (TLE)
Creation date: Sept. 3, 2025, 2:21 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 2, 2025, 9:41 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22617U 93016AB 25245.90371822 .00001300 00000-0 97850-3 0 9993
TLE line 2: 2 22617 71.0012 324.0390 0134090 210.9086 267.2921 13.91994344640539
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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