ALOUETTE 1 (S-27), 424
Orbit data source: Space-Track
ALOUETTE 1 (S-27), 424 is a payload satellite owned by DRTE (CA) in LEO that was launched on Sat, 29 Sep 1962 UTC via a THOR 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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424 intel report (Beta)
ALOUETTE 1 (S-27) details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 4 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, 1.07 m |
| Radar Cross Section | 0.784 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 4 hours ago
0 ALOUETTE 1 (S-27)
1 424U 62049A 25015.14937096 .00000121 00000-0 12813-3 0 9995
2 424 80.4656 48.9727 0023845 132.6999 227.6160 13.69468468110392Epoch: 2025-01-15T03:35Z
Definitive object data (Epoch: 2025-01-15T03:35:05.65Z)
| Latitude | -0.00006° |
| Longitude | -119.64671° |
| Altitude | 1,016.185 km |
| Speed | 7.338 km/s |
| True Right ascension | 03h 15m 53s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 1.33245° |
| Longitude | 59.95034° |
| Altitude | 991.956 km |
| Speed | 7.362 km/s |
| Apparent Right ascension | 17h 16m 53s |
| Apparent Declination | -22° 21' 29" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 08:37:09 |
| Azimuth | 82.835° E |
| Elevation | -44.377° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 1,016.337 km |
| Perigee altitude | 981.157 km |
| Semi-major axis | 7,376.884 km |
| Eccentricity | 0.0023845 |
| Inclination | 80.4656° |
| RAAN | 48.9727° |
| Arg. of periapsis | 132.6999° |
| True anomaly | 227.41458° |
| Mean anomaly | 227.616° |
| Eccentric anomaly | 227.51525° |
| Mean motion | 3.42558 °/min |
| BSTAR | 0.00012813 |
| Orbital period | 105.09 mins |
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Other satellites on launch #49 in the year 1962 (1962-09-29 UTC)
| ALOUETTE 1 (S-27), 424 |
| THOR AGENA B R/B, 426 |
| THOR AGENA B DEB, 510 |
| THOR AGENA B DEB, 511 |
ALOUETTE 1 (S-27) 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-01-15 12:55:31.893Z | 10.002° NNE | 2025-01-15 13:00:31.893Z | 63.851° ENE | 26.985° | 2025-01-15 13:05:31.893Z | 126.596° SE |
| 10 mins | 2025-01-15 14:42:31.893Z | 329.392° NNW | 2025-01-15 14:47:31.893Z | 261.053° W | 31.893° | 2025-01-15 14:52:31.893Z | 203.675° SW |
| 11 mins | 2025-01-16 02:29:31.893Z | 167.501° S | 2025-01-16 02:34:31.893Z | 90.866° ESE | 39.558° | 2025-01-16 02:40:31.893Z | 19.315° NNE |
| 8 mins | 2025-01-16 04:17:31.893Z | 252.355° W | 2025-01-16 04:21:31.893Z | 299.102° NW | 20.829° | 2025-01-16 04:25:31.893Z | 340.553° N |
Authenticating...
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