H-2A R/B, 43224 (Decayed)
Orbit data source: Space-Track
H-2A R/B, 43224 was space debris in LEO originally from a launch on Tue, 27 Feb 2018 UTC launched from the Tanegashima Space Center (TNSTA). 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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43224 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
MHI Tobishima
Mission
Decayed spacecraft
Bus & Motor
H-2A STAGE 2, Unknown motor
Mass
4,000 kg wet, 4,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 4.6 m
Radar Cross Section
35.186 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 H-2A R/B
1 43224U 18021B 24118.09334668 .25975779 24965-5 26321-3 0 9991
2 43224 97.2192 222.2039 0014138 264.2949 223.6135 16.50276103344486Epoch: 2024-04-27T02:14Z
TLE epoch observation values (Epoch: 2024-04-27T02:14:25.153Z)
Latitude
51.73193°
Longitude
162.22031°
Altitude
153.769 km
Speed
7.815 km/s
True Right ascension
03h 25m 33s
True Declination
51° 32' 57"
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
21:52:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
144.604 km
Perigee altitude
126.186 km
Semi-major axis
6,513.532 km
Eccentricity
0.00141
Inclination
97.2192°
RAAN
222.2039°
Arg. of periapsis
264.2949°
True anomaly
223.50189°
Mean anomaly
223.6135°
Eccentric anomaly
223.55768°
Mean motion
4.12875 °/min
Orbital period
87.19 mins
BSTAR
0.00026321
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Other satellites on launch #21 in the year 2018 (2018-02-27 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.H-2A 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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