ASTRO H, 41337
Orbit data source: Space-Track
ASTRO H, 41337 is a Japanese payload satellite in LEO that was launched on Wed, 17 Feb 2016 UTC via an H-IIA 202 launch vehicle from the Tanegashima Space Center (TNSTA). 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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41337 intel report (Beta)
ASTRO H details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 18 hours ago |
| Origin | |
| Manufacturer | TSUK/NECTF |
| Mission | Non-operational Civil Astronomy |
| Bus & Motor | ASTRO-H, Unknown motor |
| Mass | 2,700 kg wet, 2,700 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Oct Cyl + 2 Pan + 1 Truss, 14 m |
| Radar Cross Section | 16.262 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 18 hours ago
0 ASTRO H
1 41337U 16012A 24338.60910414 .00006630 00000-0 43704-3 0 9999
2 41337 31.0014 83.6680 0010410 28.4016 331.7187 15.06041748482568Epoch: 2024-12-03T14:37Z
Definitive object data (Epoch: 2024-12-03T14:37:06.597Z)
| Latitude | -0.00002° |
| Longitude | 151.47433° |
| Altitude | 540.476 km |
| Speed | 7.598 km/s |
| True Right ascension | 05h 34m 40s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 20.02871° |
| Longitude | -70.47305° |
| Altitude | 547.931 km |
| Speed | 7.591 km/s |
| Apparent Right ascension | 16h 24m 31s |
| Apparent Declination | -9° 41' 50" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 06:37:45 |
| Azimuth | 53.579° ENE |
| Elevation | -47.723° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 559.358 km |
| Perigee altitude | 544.929 km |
| Semi-major axis | 6,930.281 km |
| Eccentricity | 0.001041 |
| Inclination | 31.0014° |
| RAAN | 83.668° |
| Arg. of periapsis | 28.4016° |
| True anomaly | 331.66212° |
| Mean anomaly | 331.7187° |
| Eccentric anomaly | 331.69041° |
| Mean motion | 3.76198 °/min |
| BSTAR | 0.00043704 |
| Orbital period | 95.69 mins |
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Other satellites on launch #12 in the year 2016 (2016-02-17 UTC)
ASTRO H 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 | 2024-12-04 11:34:35.760Z | 197.96° SSW | 2024-12-04 11:36:35.760Z | 164.336° S | 16.481° | 2024-12-04 11:38:35.760Z | 131.891° SE |
| 4 mins | 2024-12-04 13:15:35.760Z | 212.116° SW | 2024-12-04 13:17:35.760Z | 169.629° S | 21.215° | 2024-12-04 13:19:35.760Z | 135.285° SSE |
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