ALOUETTE 2, 1804
Orbit data source: Space-Track
ALOUETTE 2, 1804 is a payload satellite owned by DRTE (CA) in LEO that was launched on Mon, 29 Nov 1965 UTC via a THOR SLV-2 AGENA B launch vehicle from the Air Force Western Test Range (AFWTR). 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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1804 intel report (Beta)
ALOUETTE 2 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 11 hours ago |
| Origin | |
| Manufacturer | DEHAVT/RCAV |
| Mission | Civil Science |
| Bus & Motor | ALOUETTE, Unknown motor |
| Mass | 145 kg wet, 145 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Ell + 1 Rod, 73 m |
| Radar Cross Section | 0.732 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 11 hours ago
0 ALOUETTE 2
1 1804U 65098A 24356.07531288 .00001298 00000-0 43226-3 0 9995
2 1804 79.8035 18.4104 1332864 253.1035 92.0019 12.27544688612200Epoch: 2024-12-21T01:48Z
Definitive object data (Epoch: 2024-12-21T01:48:27.032Z)
| Latitude | -0.00004° |
| Longitude | -98.83392° |
| Altitude | 1,737.717 km |
| Speed | 6.932 km/s |
| True Right ascension | 01h 13m 38s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -69.69899° |
| Longitude | -128.15301° |
| Altitude | 683.016 km |
| Speed | 7.932 km/s |
| Apparent Right ascension | 23h 54m 15s |
| Apparent Declination | -55° 36' 21" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:13:11 |
| Azimuth | 170.264° S |
| Elevation | -74° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 2,614.954 km |
| Perigee altitude | 499.59 km |
| Semi-major axis | 7,935.409 km |
| Eccentricity | 0.1332864 |
| Inclination | 79.8035° |
| RAAN | 18.4104° |
| Arg. of periapsis | 253.1035° |
| True anomaly | 107.00466° |
| Mean anomaly | 92.0019° |
| Eccentric anomaly | 99.53318° |
| Mean motion | 3.07036 °/min |
| BSTAR | 0.00043226 |
| Orbital period | 117.25 mins |
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Other satellites on launch #98 in the year 1965 (1965-11-29 UTC)
ALOUETTE 2 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. |
|---|---|---|---|---|---|---|---|
| 19 mins | 2024-12-21 14:16:15.589Z | 340.849° N | 2024-12-21 14:27:15.589Z | 280.367° WNW | 37.393° | 2024-12-21 14:35:15.589Z | 203.381° SW |
| 23 mins | 2024-12-22 01:22:15.589Z | 150.297° SSE | 2024-12-22 01:32:15.589Z | 83.299° E | 36.456° | 2024-12-22 01:45:15.589Z | 20.178° NNE |
| 25 mins | 2024-12-22 03:20:15.589Z | 214.609° SW | 2024-12-22 03:30:15.589Z | 284.892° WNW | 40.572° | 2024-12-22 03:45:15.589Z | 7.15° NNE |
| 16 mins | 2024-12-22 05:26:15.589Z | 281.089° WNW | 2024-12-22 05:33:15.589Z | 313.564° NW | 17.805° | 2024-12-22 05:42:15.589Z | 352.396° N |
| 18 mins | 2024-12-22 11:46:15.589Z | 1.903° NNE | 2024-12-22 11:56:15.589Z | 59.646° ENE | 29.239° | 2024-12-22 12:04:15.589Z | 119.839° SE |
Authenticating...
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