Key statistics
Satellite SL-16 DEB at a glance.
Uptime
10906
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: 104.778 minutes
Inclination: 70.9979 deg
SMA: 7362.188 km
Apoapsis: 1128.677 km
Periapsis: 839.429 km
RAAN: 268.2193 deg
Eccentricy: 0.01964415
Argument of periapsis: 83.7013 deg
Mean anomaly: 78.1 deg
Mean motion: 13.74334474 rev/day
Mean motion (dot): 0.00000098 rev/day2
B* drag term: 0.00012917259 1/REarth
Two-line elements (TLE)
Creation date: Sept. 8, 2025, 6:18 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 8, 2025, 11:33 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23706U 95058C 25251.48148419 .00000098 00000-0 12917-3 0 9999
TLE line 2: 2 23706 70.9979 268.2193 0196442 83.7013 78.1000 13.74334474496612
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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