Key statistics
Satellite SL-16 DEB at a glance.
Uptime
10952
Days in orbit
Revolutions
≈ 13.8
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: 1995-058E
Object number (NORAD): 23708
Object ID (CCSDS): 23708
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.6 minutes
Inclination: 71.0488 deg
SMA: 7353.866 km
Apoapsis: 1112.97 km
Periapsis: 838.492 km
RAAN: 144.5355 deg
Eccentricy: 0.01866216
Argument of periapsis: 231.0352 deg
Mean anomaly: 246.5777 deg
Mean motion: 13.76668017 rev/day
Mean motion (dot): 0.00000089 rev/day2
B* drag term: 0.00011867986 1/REarth
Two-line elements (TLE)
Creation date: Oct. 25, 2025, 3:11 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 24, 2025, 11:56 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23708U 95058E 25297.99731991 .00000089 00000-0 11868-3 0 9994
TLE line 2: 2 23708 71.0488 144.5355 0186622 231.0352 246.5777 13.76668017505742
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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