Key statistics
Satellite SL-16 DEB at a glance.
Uptime
10841
Days in orbit
Revolutions
≈ 14.2
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.9
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: 1995-058G
Object number (NORAD): 24284
Object ID (CCSDS): 24284
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.389 minutes
Inclination: 70.8628 deg
SMA: 7202.548 km
Apoapsis: 834.468 km
Periapsis: 814.358 km
RAAN: 60.2513 deg
Eccentricy: 0.0013961
Argument of periapsis: 292.3723 deg
Mean anomaly: 67.5922 deg
Mean motion: 14.2027853 rev/day
Mean motion (dot): 0.00000067 rev/day2
B* drag term: 0.000054267 1/REarth
Two-line elements (TLE)
Creation date: July 5, 2025, 10:46 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 5, 2025, 6:54 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 24284U 95058G 25186.78774895 .00000067 00000-0 54267-4 0 9995
TLE line 2: 2 24284 70.8628 60.2513 0013961 292.3723 67.5922 14.20278530534913
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
In-orbit conjunctions
A list of the most updated potential collisions computed for object 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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