Key statistics
Satellite SL-16 DEB at a glance.
Uptime
10534
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: 1996-051D
Object number (NORAD): 24300
Object ID (CCSDS): 24300
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.753 minutes
Inclination: 71.0283 deg
SMA: 7361.002 km
Apoapsis: 1127.414 km
Periapsis: 838.321 km
RAAN: 70.7506 deg
Eccentricy: 0.0196368
Argument of periapsis: 220.0938 deg
Mean anomaly: 292.1861 deg
Mean motion: 13.74666406 rev/day
Mean motion (dot): 0.00000053 rev/day2
B* drag term: 0.000088629 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 2:35 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 24300U 96051D 25187.10828258 .00000053 00000-0 88629-4 0 9992
TLE line 2: 2 24300 71.0283 70.7506 0196368 220.0938 292.1861 13.74666406445728
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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