Key statistics
Satellite SL-16 DEB at a glance.
Uptime
13928
Days in orbit
Revolutions
≈ 13.8
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: 1987-027F
Object number (NORAD): 18550
Object ID (CCSDS): 18550
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.413 minutes
Inclination: 71.0245 deg
SMA: 7345.063 km
Apoapsis: 1101.444 km
Periapsis: 832.412 km
RAAN: 255.317 deg
Eccentricy: 0.0183138
Argument of periapsis: 304.6871 deg
Mean anomaly: 53.7093 deg
Mean motion: 13.79143503 rev/day
Mean motion (dot): 0.00000136 rev/day2
B* drag term: 0.00015507 1/REarth
Two-line elements (TLE)
Creation date: May 5, 2025, 2:11 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 4, 2025, 7:32 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 18550U 87027F 25124.81456431 .00000136 00000-0 15507-3 0 9990
TLE line 2: 2 18550 71.0245 255.3170 0183138 304.6871 53.7093 13.79143503917679
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
Associated space launch
Dynamic simulator of the Tselina-2 ELINT satellite
SL-16 DEB was lifted into orbit during the mission ‘Zenit-2 | GVM Tselina-2’, on board a Zenit-2 space rocket.
The launch took place on March 18, 1987, 8:30 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | GVM Tselina-2
Agency: N/A
Status: Launch Successful
Launch date: March 18, 1987, 8:30 a.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.
