Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11730
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: 103.166 minutes
Inclination: 70.9926 deg
SMA: 7286.464 km
Apoapsis: 996.78 km
Periapsis: 819.879 km
RAAN: 353.7492 deg
Eccentricy: 0.012139
Argument of periapsis: 227.6281 deg
Mean anomaly: 131.4506 deg
Mean motion: 13.95813811 rev/day
Mean motion (dot): 0.00000717 rev/day2
B* drag term: 0.00052481 1/REarth
Two-line elements (TLE)
Creation date: April 14, 2025, 3:05 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: April 13, 2025, 10:27 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39895U 93016BV 25103.43557798 .00000717 00000-0 52481-3 0 9990
TLE line 2: 2 39895 70.9926 353.7492 0121390 227.6281 131.4506 13.95813811273941
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
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