CHUBUSAT 3, 41339
Orbit data source: Space-Track
CHUBUSAT 3, 41339 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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41339 intel report (Beta)
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CHUBUSAT 3 radio frequencies
CHUBUSAT 3 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 13 hours ago |
| Origin | |
| Manufacturer | NAG/MHIME |
| Mission | Non-operational Amateur Imaging |
| Bus & Motor | Unknown |
| Mass | 52 kg wet, 52 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box, 0.6 m |
| Radar Cross Section | 0.480 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 13 hours ago
0 CHUBUSAT 3
1 41339U 16012C 24360.99248864 .00009681 00000-0 55164-3 0 9993
2 41339 31.0055 232.6885 0010871 7.0688 353.0103 15.11471761486496Epoch: 2024-12-25T23:49Z
Definitive object data (Epoch: 2024-12-25T23:49:11.018Z)
| Latitude | 0.00001° |
| Longitude | 140.41433° |
| Altitude | 522.766 km |
| Speed | 7.608 km/s |
| True Right ascension | 15h 30m 45s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 28.17835° |
| Longitude | -105.57126° |
| Altitude | 532.198 km |
| Speed | 7.601 km/s |
| Apparent Right ascension | 23h 40m 06s |
| Apparent Declination | -4° 21' 05" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:21:37 |
| Azimuth | 17.46° NNE |
| Elevation | -53.22° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 543.069 km |
| Perigee altitude | 528.038 km |
| Semi-major axis | 6,913.691 km |
| Eccentricity | 0.0010871 |
| Inclination | 31.0055° |
| RAAN | 232.6885° |
| Arg. of periapsis | 7.0688° |
| True anomaly | 352.99512° |
| Mean anomaly | 353.0103° |
| Eccentric anomaly | 353.00271° |
| Mean motion | 3.77553 °/min |
| BSTAR | 0.00055164 |
| Orbital period | 95.35 mins |
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Other satellites on launch #12 in the year 2016 (2016-02-17 UTC)
CHUBUSAT 3 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 20:45:01.512Z | 194.386° SSW | 2024-12-26 20:46:01.512Z | 174.162° S | 19.205° | 2024-12-26 20:49:01.512Z | 124.53° SE |
| 4 mins | 2024-12-26 22:25:01.512Z | 214.507° SW | 2024-12-26 22:26:01.512Z | 194.81° SSW | 19.873° | 2024-12-26 22:29:01.512Z | 140.625° SSE |
Authenticating...
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