Key statistics
Satellite SL-16 DEB at a glance.
Uptime
13441
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: 1988-102E
Object number (NORAD): 19658
Object ID (CCSDS): 19658
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.728 minutes
Inclination: 71.0197 deg
SMA: 7359.869 km
Apoapsis: 1125.188 km
Periapsis: 838.28 km
RAAN: 296.9645 deg
Eccentricy: 0.01949137
Argument of periapsis: 52.8093 deg
Mean anomaly: 14.3333 deg
Mean motion: 13.74983968 rev/day
Mean motion (dot): 0.00000097 rev/day2
B* drag term: 0.00012705389 1/REarth
Two-line elements (TLE)
Creation date: Sept. 9, 2025, 10:35 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 9, 2025, 3:45 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 19658U 88102E 25252.15640426 .00000097 00000-0 12705-3 0 9996
TLE line 2: 2 19658 71.0197 296.9645 0194914 52.8093 14.3333 13.74983968844968
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 6’, on board a Zenit-2 space rocket.
The launch took place on Nov. 23, 1988, 2:50 p.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 6
Agency: N/A
Status: Launch Successful
Launch date: Nov. 23, 1988, 2:50 p.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
...
Latest news about this satellite
There are no fresh news available about this satellite. Check back as we update our databases every day.
Newsletter sign-up
Weekly statistics, charts and insights to help you stay on top of the space industry.
