HODOYOSHI 1, 40299
Orbit data source: Space-Track
HODOYOSHI 1, 40299 is a Japanese payload satellite in LEO that was launched on Thu, 06 Nov 2014 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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40299 intel report (Beta)
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HODOYOSHI 1 radio frequencies
HODOYOSHI 1 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 10 hours ago |
| Origin | |
| Manufacturer | AXELSPACE |
| Mission | Operational Commercial Imaging |
| Bus & Motor | HODOYOSHI, Unknown motor |
| Mass | 50 kg wet, 50 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 2 Pan, 1.5 m |
| Radar Cross Section | 0.614 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 10 hours ago
0 HODOYOSHI 1
1 40299U 14070B 24336.86999561 .00104144 00000-0 89133-3 0 9998
2 40299 97.1121 36.7144 0005386 134.5505 225.6198 15.69106702561188Epoch: 2024-12-01T20:52Z
Definitive object data (Epoch: 2024-12-01T20:52:47.62Z)
| Latitude | -0.00004° |
| Longitude | 12.31398° |
| Altitude | 367.159 km |
| Speed | 7.688 km/s |
| True Right ascension | 02h 26m 51s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -50.76571° |
| Longitude | 21.49762° |
| Altitude | 384.613 km |
| Speed | 7.676 km/s |
| Apparent Right ascension | 21h 12m 23s |
| Apparent Declination | -74° 40' 56" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 05:08:36 |
| Azimuth | 199.355° SSW |
| Elevation | -45.829° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 361.97 km |
| Perigee altitude | 354.714 km |
| Semi-major axis | 6,736.479 km |
| Eccentricity | 0.0005386 |
| Inclination | 97.1121° |
| RAAN | 36.7144° |
| Arg. of periapsis | 134.5505° |
| True anomaly | 225.57571° |
| Mean anomaly | 225.6198° |
| Eccentric anomaly | 225.59775° |
| Mean motion | 3.92549 °/min |
| BSTAR | 0.00089133 |
| Orbital period | 91.71 mins |
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Other satellites on launch #70 in the year 2014 (2014-11-06 UTC)
| ASNARO, 40298 |
| HODOYOSHI 1, 40299 |
| CHUBUSAT 1, 40300 |
| QSAT-EOS, 40301 (Decayed) |
| TSUBAME, 40302 (Decayed) |
| SL-24 R/B, 40303 |
| SL-24 PLAT, 40304 (Decayed) |
HODOYOSHI 1 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2024-12-02 17:19:32.678Z | 357.455° N | 2024-12-02 17:21:32.678Z | 315.221° NNW | 33.272° | 2024-12-02 17:24:32.678Z | 210.709° SW |
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