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). Payload-class satellites include a variety of spacecraft 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)
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Edit Public Description
Identifier
Orbit
Country
CARelated business
Manufacturer
DEHAVT/RCAV
Mission
Spacecraft
Bus & Motor
ALOUETTE, Unknown motor
Mass
145 kg wet, 145 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 ALOUETTE 1 (S-27)
1 424U 62049A 25312.49153330 .00000134 00000-0 14341-3 0 9996
2 424 80.4640 114.7814 0023496 86.9924 273.3910 13.69544169150900Epoch: 2025-11-08T11:47Z
TLE epoch observation values (Epoch: 2025-11-08T11:47:48.477Z)
Latitude
-0°
Longitude
-110.09097°
Altitude
1,003.041 km
Speed
7.351 km/s
True Right ascension
07h 39m 07s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
17:39:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,015.807 km
Perigee altitude
981.143 km
Semi-major axis
7,376.612 km
Eccentricity
0.00235
Inclination
80.464°
RAAN
114.7814°
Arg. of periapsis
86.9924°
True anomaly
273.12218°
Mean anomaly
273.391°
Eccentric anomaly
273.2566°
Mean motion
3.42577 °/min
Orbital period
105.09 mins
BSTAR
0.00014341
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Other satellites on launch #49 in the year 1962 (1962-09-29 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ALOUETTE 1 (S-27) Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-11-08 22:53:53.099Z | 346.854° N | 2025-11-08 22:59:53.099Z | 231.157° WSW | 44.337° | 2025-11-08 23:05:53.099Z | 176.493° S |
| 9 mins | 2025-11-09 10:42:53.099Z | 137.097° SSE | 2025-11-09 10:46:53.099Z | 89.76° E | 24.483° | 2025-11-09 10:51:53.099Z | 34.994° NE |
| 9 mins | 2025-11-09 12:28:53.099Z | 223.975° SW | 2025-11-09 12:32:53.099Z | 285.455° WNW | 34.633° | 2025-11-09 12:37:53.099Z | 353.45° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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