EPSILON R/B, 43936 (Decayed)
Orbit data source: Space-Track
EPSILON R/B, 43936 was space debris in LEO originally from a launch on Fri, 18 Jan 2019 UTC launched from the Kagoshima Space Center University Of Tokyo (KSCUT). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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43936 intel report (Beta)
EPSILON R/B details
Identifier | |
Orbit | Decayed |
Last TLE update | 1 month ago |
Origin | |
Manufacturer | JAXA |
Mission | Decayed spacecraft |
Bus & Motor | EPBS, Unknown motor |
Mass | ~185 kg wet, ~185 kg dry |
Launch date (UTC) | |
Launch vehicle | Unknown |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Cyl, 1.5 m |
Radar Cross Section | 2.297 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 1 month ago
0 EPSILON R/B
1 43936U 19003E 24316.94575978 .17950001 23612-5 27064-3 0 9992
2 43936 97.0227 336.1311 0008488 267.9293 140.8430 16.48315615325266
Epoch: 2024-11-11T22:41Z
Definitive object data (Epoch: 2024-11-11T22:41:53.644Z)
Latitude | 48.45283° |
Longitude | -63.85017° |
Altitude | 155.818 km |
Speed | 7.815 km/s |
True Right ascension | 21h 52m 44s |
True Declination | 48° 15' 59" |
Sunlit | Object was in full shadow at TLE epoch |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
Apogee altitude | 146.088 km |
Perigee altitude | 135.022 km |
Semi-major axis | 6,518.692 km |
Eccentricity | 0.0008488 |
Inclination | 97.0227° |
RAAN | 336.1311° |
Arg. of periapsis | 267.9293° |
True anomaly | 140.90437° |
Mean anomaly | 140.843° |
Eccentric anomaly | 140.87369° |
Mean motion | 4.12385 °/min |
BSTAR | 0.00027064 |
Orbital period | 87.3 mins |
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Other satellites on launch #3 in the year 2019 (2019-01-18 UTC)
EPSILON R/B Visibility forecast
Observer location: undefined°, undefined
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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