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 | 7 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 7 hours ago
0 ALOUETTE 1 (S-27)
1 424U 62049A 25014.12653950 .00000129 00000-0 13741-3 0 9995
2 424 80.4657 49.9849 0023821 135.2598 225.0475 13.69468241110252Epoch: 2025-01-14T03:02Z
Definitive object data (Epoch: 2025-01-14T03:02:13.012Z)
| Latitude | -0° |
| Longitude | -109.40702° |
| Altitude | 1,016.742 km |
| Speed | 7.337 km/s |
| True Right ascension | 03h 19m 56s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -75.03066° |
| Longitude | 109.00174° |
| Altitude | 1,038.427 km |
| Speed | 7.327 km/s |
| Apparent Right ascension | 21h 02m 15s |
| Apparent Declination | -61° 51' 36" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 10:09:06 |
| Azimuth | 160.663° S |
| Elevation | -65.821° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 1,016.32 km |
| Perigee altitude | 981.175 km |
| Semi-major axis | 7,376.885 km |
| Eccentricity | 0.0023821 |
| Inclination | 80.4657° |
| RAAN | 49.9849° |
| Arg. of periapsis | 135.2598° |
| True anomaly | 224.85473° |
| Mean anomaly | 225.0475° |
| Eccentric anomaly | 224.95107° |
| Mean motion | 3.42558 °/min |
| BSTAR | 0.00013741 |
| 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-01-14 12:24:09.295Z | 33.58° NE | 2025-01-14 12:27:09.295Z | 63.705° ENE | 14.33° | 2025-01-14 12:30:09.295Z | 93.425° ESE |
| 11 mins | 2025-01-14 14:09:09.295Z | 347.544° N | 2025-01-14 14:14:09.295Z | 257.556° W | 44.785° | 2025-01-14 14:20:09.295Z | 174.854° S |
| 8 mins | 2025-01-15 01:58:09.295Z | 129.686° SE | 2025-01-15 02:01:09.295Z | 93.288° ESE | 23.688° | 2025-01-15 02:06:09.295Z | 37.264° NE |
| 10 mins | 2025-01-15 03:43:09.295Z | 220.709° SW | 2025-01-15 03:47:09.295Z | 278.686° WNW | 35.695° | 2025-01-15 03:53:09.295Z | 357.347° N |
Authenticating...
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