Key statistics
Satellite SL-16 DEB at a glance.
Uptime
10595
Days in orbit
Revolutions
≈ 13.7
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: 1996-051E
Object number (NORAD): 24301
Object ID (CCSDS): 24301
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.916 minutes
Inclination: 70.996 deg
SMA: 7368.661 km
Apoapsis: 1143.897 km
Periapsis: 837.155 km
RAAN: 345.8473 deg
Eccentricy: 0.02081393
Argument of periapsis: 218.8497 deg
Mean anomaly: 264.9925 deg
Mean motion: 13.72523803 rev/day
Mean motion (dot): 0.0000014 rev/day2
B* drag term: 0.00017184318 1/REarth
Two-line elements (TLE)
Creation date: Sept. 7, 2025, 3:09 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 6, 2025, 4:10 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 24301U 96051E 25249.67385654 .00000140 00000-0 17184-3 0 9996
TLE line 2: 2 24301 70.9960 345.8473 0208139 218.8497 264.9925 13.72523803452067
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 18’, on board a Zenit-2 space rocket.
The launch took place on Sept. 4, 1996, 9:01 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 18
Agency: N/A
Status: Launch Successful
Launch date: Sept. 4, 1996, 9:01 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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