Key statistics
Satellite SL-16 DEB at a glance.
Uptime
13992
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: 1987-027D
Object number (NORAD): 18417
Object ID (CCSDS): 18417
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.76 minutes
Inclination: 70.9999 deg
SMA: 7361.359 km
Apoapsis: 1130.692 km
Periapsis: 835.755 km
RAAN: 299.8764 deg
Eccentricy: 0.0200328
Argument of periapsis: 46.7702 deg
Mean anomaly: 24.8704 deg
Mean motion: 13.74566589 rev/day
Mean motion (dot): -0.00000028 rev/day2
B* drag term: 0.00001257 1/REarth
Two-line elements (TLE)
Creation date: July 8, 2025, 2:27 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 7, 2025, 5:29 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 18417U 87027D 25188.72882125 -.00000028 00000-0 12570-4 0 9994
TLE line 2: 2 18417 70.9999 299.8764 0200328 46.7702 24.8704 13.74566589920181
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
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