Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11183
Days in orbit
Revolutions
≈ 14.1
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: 1994-077J
Object number (NORAD): 23418
Object ID (CCSDS): 23418
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.112 minutes
Inclination: 71.0038 deg
SMA: 7236.769 km
Apoapsis: 913.871 km
Periapsis: 803.397 km
RAAN: 179.0589 deg
Eccentricy: 0.0076328
Argument of periapsis: 345.0588 deg
Mean anomaly: 14.8276 deg
Mean motion: 14.10216269 rev/day
Mean motion (dot): 0.00000232 rev/day2
B* drag term: 0.00015343 1/REarth
Two-line elements (TLE)
Creation date: July 3, 2025, 3:40 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 2, 2025, 5:10 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23418U 94077J 25183.71547092 .00000232 00000-0 15343-3 0 9995
TLE line 2: 2 23418 71.0038 179.0589 0076328 345.0588 14.8276 14.10216269614176
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 16’, on board a Zenit-2 space rocket.
The launch took place on Nov. 24, 1994, 9:15 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 16
Agency: N/A
Status: Launch Successful
Launch date: Nov. 24, 1994, 9:15 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
...
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