Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11790
Days in orbit
Revolutions
≈ 14.4
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: 1993-016BR
Object number (NORAD): 39891
Object ID (CCSDS): 39891
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.814 minutes
Inclination: 70.9972 deg
SMA: 7127.794 km
Apoapsis: 756.183 km
Periapsis: 743.135 km
RAAN: 266.5097 deg
Eccentricy: 0.0009153
Argument of periapsis: 20.7362 deg
Mean anomaly: 339.4145 deg
Mean motion: 14.4268004 rev/day
Mean motion (dot): 0.00001235 rev/day2
B* drag term: 0.00038605 1/REarth
Two-line elements (TLE)
Creation date: July 4, 2025, 6:39 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 4, 2025, 1:42 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39891U 93016BR 25185.57146016 .00001235 00000-0 38605-3 0 9996
TLE line 2: 2 39891 70.9972 266.5097 0009153 20.7362 339.4145 14.42680040580066
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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