EPSILON R/B, 43153 (Decayed)
Orbit data source: Space-Track
EPSILON R/B, 43153 was space debris in LEO originally from a launch on Wed, 17 Jan 2018 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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43153 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
JP / JPNRelated business
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
Shape & HBR
Cyl, 0.8 m
Radar Cross Section
2.297 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 EPSILON R/B
1 43153U 18007B 24235.72727729 .39980158 26350-5 15933-3 0 9999
2 43153 97.2870 270.8298 0011327 255.7088 199.7159 16.57586518369344Epoch: 2024-08-22T17:27Z
TLE epoch observation values (Epoch: 2024-08-22T17:27:16.757Z)
Latitude
80.99763°
Longitude
-89.13351°
Altitude
139.811 km
Speed
7.825 km/s
True Right ascension
09h 36m 47s
True Declination
80° 56' 21"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
11:10:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
123.57 km
Perigee altitude
108.858 km
Semi-major axis
6,494.351 km
Eccentricity
0.00113
Inclination
97.287°
RAAN
270.8298°
Arg. of periapsis
255.7088°
True anomaly
199.67217°
Mean anomaly
199.7159°
Eccentric anomaly
199.69403°
Mean motion
4.14705 °/min
Orbital period
86.81 mins
BSTAR
0.00015933
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Other satellites on launch #7 in the year 2018 (2018-01-17 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.EPSILON R/B Visibility
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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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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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