HODOYOSHI 1, 40299
Orbit data source: Space-Track
HODOYOSHI 1, 40299 is a Japanese payload satellite in SSO 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 | SSO |
| Last TLE update | 8 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 8 hours ago
0 HODOYOSHI 1
1 40299U 14070B 24361.12894445 .00118312 00000-0 81608-3 0 9991
2 40299 97.1075 61.4248 0004489 54.4944 305.6739 15.74222770565012Epoch: 2024-12-26T03:05Z
Definitive object data (Epoch: 2024-12-26T03:05:40.8Z)
| Latitude | -0.00006° |
| Longitude | -80.10797° |
| Altitude | 348.256 km |
| Speed | 7.701 km/s |
| True Right ascension | 04h 05m 41s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -22.35113° |
| Longitude | 97.33122° |
| Altitude | 357.818 km |
| Speed | 7.692 km/s |
| Apparent Right ascension | 18h 50m 10s |
| Apparent Declination | -44° 01' 30" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 10:56:06 |
| Azimuth | 116.337° SE |
| Elevation | -45.172° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 346.742 km |
| Perigee altitude | 340.707 km |
| Semi-major axis | 6,721.862 km |
| Eccentricity | 0.0004489 |
| Inclination | 97.1075° |
| RAAN | 61.4248° |
| Arg. of periapsis | 54.4944° |
| True anomaly | 305.6321° |
| Mean anomaly | 305.6739° |
| Eccentric anomaly | 305.653° |
| Mean motion | 3.9383 °/min |
| BSTAR | 0.00081608 |
| Orbital period | 91.41 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2024-12-26 17:22:43.671Z | 354.829° N | 2024-12-26 17:24:43.671Z | 287.064° WNW | 35.477° | 2024-12-26 17:26:43.671Z | 214.565° SW |
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