INTELSAT 31, 41581
Orbit data source: Space-Track
INTELSAT 31, 41581 is an American payload satellite in GEO that was launched on Thu, 09 Jun 2016 UTC via a PROTON-M/BRIZ-M launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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41581 intel report (Beta)
INTELSAT 31 details
| Identifier | |
| Orbit | GEO |
| Last TLE update | 6 days ago |
| Origin | |
| Manufacturer | SS/Loral (MDA) |
| Mission | Operational Commercial Communications |
| Bus & Motor | LS-1300S, R-4D-11 |
| Mass | 6,450 kg wet, 3,000 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 2 Pan, Unknown HBR |
| Radar Cross Section | 55.801 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 6 days ago
0 INTELSAT 31
1 41581U 16035A 24331.54979954 -.00000130 00000-0 00000-0 0 9994
2 41581 0.0098 315.2989 0001850 212.0271 1.4980 1.00270415 31000Epoch: 2024-11-26T13:11Z
Definitive object data (Epoch: 2024-11-26T13:11:42.68Z)
| Latitude | -0.01978° |
| Longitude | -95.08754° |
| Altitude | 35,778.702 km |
| Speed | 3.075 km/s |
| True Right ascension | 11h 15m 11s |
| True Declination | 0° 01' 11" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 0.02225° |
| Longitude | 175.88036° |
| Altitude | 35,786.36 km |
| Speed | 3.075 km/s |
| Apparent Right ascension | 05h 24m 16s |
| Apparent Declination | -6° 11' 44" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 04:39:10 |
| Azimuth | 164.659° S |
| Elevation | 42.73° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 35,795.85 km |
| Perigee altitude | 35,780.249 km |
| Semi-major axis | 42,166.186 km |
| Eccentricity | 0.000185 |
| Inclination | 0.0098° |
| RAAN | 315.2989° |
| Arg. of periapsis | 212.0271° |
| True anomaly | 1.49855° |
| Mean anomaly | 1.498° |
| Eccentric anomaly | 1.49828° |
| Mean motion | 0.25067 °/min |
| BSTAR | Unknown |
| Orbital period | 1436.17 mins |
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41581 neighbors
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Other satellites on launch #35 in the year 2016 (2016-06-09 UTC)
| INTELSAT 31, 41581 |
| BREEZE-M R/B, 41582 |
| BREEZE-M DEB (TANK), 41583 |
INTELSAT 31 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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2024-12-02 06:53:11.992Z | 164.664° S | 2024-12-03 06:05:11.992Z | 164.672° S | 34.152° | 2024-12-03 06:53:11.992Z | 164.673° S |
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