Key statistics
Satellite SL-16 DEB at a glance.
Uptime
10841
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: 1995-058C
Object number (NORAD): 23706
Object ID (CCSDS): 23706
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.779 minutes
Inclination: 71.0007 deg
SMA: 7362.253 km
Apoapsis: 1130.462 km
Periapsis: 837.774 km
RAAN: 35.5826 deg
Eccentricy: 0.0198776
Argument of periapsis: 176.5192 deg
Mean anomaly: 249.6183 deg
Mean motion: 13.74316141 rev/day
Mean motion (dot): 0.00000101 rev/day2
B* drag term: 0.00013192 1/REarth
Two-line elements (TLE)
Creation date: July 5, 2025, 5:45 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 5, 2025, 2:40 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23706U 95058C 25186.61169752 .00000101 00000-0 13192-3 0 9995
TLE line 2: 2 23706 71.0007 35.5826 0198776 176.5192 249.6183 13.74316141487703
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 17’, on board a Zenit-2 space rocket.
The launch took place on Oct. 31, 1995, 8:19 p.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 17
Agency: N/A
Status: Launch Successful
Launch date: Oct. 31, 1995, 8:19 p.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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