Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11729
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: 99.832 minutes
Inclination: 71.0 deg
SMA: 7128.653 km
Apoapsis: 756.741 km
Periapsis: 744.295 km
RAAN: 39.5044 deg
Eccentricy: 0.000873
Argument of periapsis: 138.7317 deg
Mean anomaly: 221.4481 deg
Mean motion: 14.42419403 rev/day
Mean motion (dot): 0.00003365 rev/day2
B* drag term: 0.0010308 1/REarth
Two-line elements (TLE)
Creation date: May 6, 2025, 3:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 5, 2025, 12:51 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39891U 93016BR 25125.03562976 .00003365 00000-0 10308-2 0 9993
TLE line 2: 2 39891 71.0000 39.5044 0008730 138.7317 221.4481 14.42419403571336
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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