Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11790
Days in orbit
Revolutions
≈ 14.0
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: 1993-016BV
Object number (NORAD): 39895
Object ID (CCSDS): 39895
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.16 minutes
Inclination: 70.9879 deg
SMA: 7286.178 km
Apoapsis: 995.626 km
Periapsis: 820.459 km
RAAN: 196.3138 deg
Eccentricy: 0.0120205
Argument of periapsis: 114.6595 deg
Mean anomaly: 246.7091 deg
Mean motion: 13.95896208 rev/day
Mean motion (dot): 0.00000189 rev/day2
B* drag term: 0.00016104 1/REarth
Two-line elements (TLE)
Creation date: June 30, 2025, 3:44 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: June 29, 2025, 6:12 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39895U 93016BV 25180.75860973 .00000189 00000-0 16104-3 0 9997
TLE line 2: 2 39895 70.9879 196.3138 0120205 114.6595 246.7091 13.95896208284732
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 13’, on board a Zenit-2 space rocket.
The launch took place on March 26, 1993, 2:21 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 13
Agency: N/A
Status: Launch Successful
Launch date: March 26, 1993, 2:21 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.
