Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11002
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: 104.747 minutes
Inclination: 71.0371 deg
SMA: 7360.743 km
Apoapsis: 1129.46 km
Periapsis: 835.756 km
RAAN: 111.1355 deg
Eccentricy: 0.01995069
Argument of periapsis: 259.6695 deg
Mean anomaly: 116.1632 deg
Mean motion: 13.74739019 rev/day
Mean motion (dot): 0.00000246 rev/day2
B* drag term: 0.00026406842 1/REarth
Two-line elements (TLE)
Creation date: Dec. 11, 2025, 7:14 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 11, 2025, 2:50 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23709U 95058F 25345.61863200 .00000246 00000-0 26407-3 0 9997
TLE line 2: 2 23709 71.0371 111.1355 0199507 259.6695 116.1632 13.74739019509954
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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