INTELSAT 29E, 41308
Orbit data source: Space-Track
INTELSAT 29E, 41308 is a payload satellite owned by Intelsat SA (US) (US) in GEO that was launched on Wed, 27 Jan 2016 UTC via an ARIANE 5ECA launch vehicle from the French Guiana (FRGUI). 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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41308 intel report (Beta)
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INTELSAT 29E details
| Identifier | |
| Orbit | GEO |
| Last TLE update | 4 hours ago |
| Origin | |
| Manufacturer | Boeing/ES |
| Mission | Non-operational Commercial Communications |
| Bus & Motor | BSS-702MP, LEROS |
| Mass | 6,552 kg wet, ~2,946 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 2 Pan, 44 m |
| Radar Cross Section | 59.953 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 4 hours ago
0 INTELSAT 29E
1 41308U 16004A 24292.18827282 -.00000239 00000-0 00000+0 0 9998
2 41308 4.9659 77.5919 0004933 54.1345 279.8357 1.00617001 32147Epoch: 2024-10-18T04:31Z
Definitive object data (Epoch: 2024-10-18T04:31:06.771Z)
| Latitude | -2.18156° |
| Longitude | -43.38024° |
| Altitude | 35,686.466 km |
| Speed | 3.078 km/s |
| True Right ascension | 03h 26m 14s |
| True Declination | -2° 10' 46" |
| Sunlit | Object was in daylight at TLE epoch |
Predictive object data (real-time)
| Latitude | 2.68054° |
| Longitude | 15.46482° |
| Altitude | 35,670.073 km |
| Speed | 3.08 km/s |
| Apparent Right ascension | 07h 46m 27s |
| Apparent Declination | -3° 01' 13" |
| Sunlit | Object is in daylight |
Predictive observer data (real-time)
| Local Sidereal Time | 03:14:26 |
| Azimuth | 106.85° ESE |
| Elevation | 14.66° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 35,711.909 km |
| Perigee | 35,670.403 km |
| Semi-major axis | 42,069.293 km |
| Eccentricity | 0.0004933 |
| Inclination | 4.9659° |
| RAAN | 77.5919° |
| Arg. of periapsis | 54.1345° |
| True anomaly | 279.78° |
| Mean anomaly | 279.8357° |
| Eccentric anomaly | 279.80785° |
| Mean motion | 0.25153 °/min |
| BSTAR | Unknown |
| Period | 1431.22 mins |
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41308 neighbors
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Other satellites on launch #4 in the year 2016 (2016-01-27 UTC)
| INTELSAT 29E, 41308 |
| ARIANE 5 R/B, 41309 |
| ARIANE 5 DEB, 44602 (Decayed) |
| INTELSAT 29E DEB, 45488 |
INTELSAT 29E Visibility forecast
Observer location: 39.9160978°, -105.1181434
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. |
|---|---|---|---|---|---|---|---|
| 730 mins | 2024-10-18 08:25:37.587Z | 106.865° ESE | 2024-10-18 11:54:37.587Z | 104.819° ESE | 15.403° | 2024-10-18 20:35:37.587Z | 110.744° ESE |
| 255 mins | 2024-10-19 04:10:37.587Z | 109.96° ESE | 2024-10-19 08:25:37.587Z | 105.824° ESE | 13.433° | 2024-10-19 08:25:37.587Z | 105.824° ESE |