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 | 1 day 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 1 day ago
0 ALOUETTE 2
1 01804U 65098A 25022.35128977 .00000734 00000-0 23963-3 0 9994
2 01804 79.8032 350.9779 1333059 187.7279 170.1261 12.27620658616571Epoch: 2025-01-22T08:25Z
Definitive object data (Epoch: 2025-01-22T08:25:51.436Z)
| Latitude | -0.00004° |
| Longitude | 102.56917° |
| Altitude | 2,608.244 km |
| Speed | 6.207 km/s |
| True Right ascension | 23h 23m 54s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -56.5996° |
| Longitude | 85.78915° |
| Altitude | 1,940.651 km |
| Speed | 6.764 km/s |
| Apparent Right ascension | 00h 30m 52s |
| Apparent Declination | -53° 53' 41" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 14:35:26 |
| Azimuth | 134.171° SE |
| Elevation | -64.857° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 2,614.738 km |
| Perigee altitude | 499.151 km |
| Semi-major axis | 7,935.082 km |
| Eccentricity | 0.1333059 |
| Inclination | 79.8032° |
| RAAN | 350.9779° |
| Arg. of periapsis | 187.7279° |
| True anomaly | 172.37404° |
| Mean anomaly | 170.1261° |
| Eccentric anomaly | 171.28357° |
| Mean motion | 3.07055 °/min |
| BSTAR | 0.00023963 |
| Orbital period | 117.24 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-01-23 19:50:22.606Z | 98.127° ESE | 2025-01-23 19:55:22.606Z | 76.375° E | 13.085° | 2025-01-23 19:59:22.606Z | 57.257° ENE |
| 24 mins | 2025-01-23 21:39:22.606Z | 165.246° S | 2025-01-23 21:52:22.606Z | 91.826° ESE | 40.585° | 2025-01-23 22:03:22.606Z | 19.531° NNE |
| 22 mins | 2025-01-23 23:39:22.606Z | 221.786° SW | 2025-01-23 23:51:22.606Z | 289.379° WNW | 35.988° | 2025-01-24 00:01:22.606Z | 357.979° N |
| 5 mins | 2025-01-24 08:07:22.606Z | 26.012° NE | 2025-01-24 08:10:22.606Z | 63.84° ENE | 17.876° | 2025-01-24 08:12:22.606Z | 93.036° ESE |
| 7 mins | 2025-01-24 10:05:22.606Z | 327.373° NNW | 2025-01-24 10:09:22.606Z | 264.6° W | 28.895° | 2025-01-24 10:12:22.606Z | 210.59° SW |
Authenticating...
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