Key statistics
Satellite SL-16 DEB at a glance.
Uptime
10788
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: 1995-058F
Object number (NORAD): 23709
Object ID (CCSDS): 23709
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.752 minutes
Inclination: 71.0361 deg
SMA: 7360.962 km
Apoapsis: 1128.849 km
Periapsis: 836.805 km
RAAN: 167.0112 deg
Eccentricy: 0.0198374
Argument of periapsis: 202.9377 deg
Mean anomaly: 310.6384 deg
Mean motion: 13.74677756 rev/day
Mean motion (dot): 0.00000156 rev/day2
B* drag term: 0.00018147 1/REarth
Two-line elements (TLE)
Creation date: May 13, 2025, 6:58 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 13, 2025, 12:56 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23709U 95058F 25133.53946615 .00000156 00000-0 18147-3 0 9997
TLE line 2: 2 23709 71.0361 167.0112 0198374 202.9377 310.6384 13.74677756480809
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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