Key statistics
Satellite SL-16 DEB at a glance.
Uptime
10473
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: 104.754 minutes
Inclination: 71.0277 deg
SMA: 7361.055 km
Apoapsis: 1127.765 km
Periapsis: 838.075 km
RAAN: 186.7961 deg
Eccentricy: 0.0196772
Argument of periapsis: 303.7543 deg
Mean anomaly: 237.7098 deg
Mean motion: 13.74651756 rev/day
Mean motion (dot): 0.00000078 rev/day2
B* drag term: 0.00011133 1/REarth
Two-line elements (TLE)
Creation date: May 8, 2025, 3:01 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 7, 2025, 10:55 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 24300U 96051D 25127.95521735 .00000078 00000-0 11133-3 0 9991
TLE line 2: 2 24300 71.0277 186.7961 0196772 303.7543 237.7098 13.74651756437599
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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