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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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: 5 hours ago
TLE from 5 hours ago
0 ALOUETTE 1 (S-27)
1 424U 62049A 26127.71585234 .00000097 00000-0 10119-3 0 9995
2 424 80.4649 296.4379 0022595 342.9690 17.0695 13.69584233175576Epoch: 2026-05-07T17:10Z
TLE epoch observation values (Epoch: 2026-05-07T17:10:49.642Z)
Latitude
0.00002°
Longitude
173.17306°
Altitude
987.944 km
Speed
7.366 km/s
True Right ascension
19h 45m 45s
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
06:40:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,014.998 km
Perigee altitude
981.664 km
Semi-major axis
7,376.468 km
Eccentricity
0.00226
Inclination
80.4649°
RAAN
296.4379°
Arg. of periapsis
342.969°
True anomaly
17.14571°
Mean anomaly
17.0695°
Eccentric anomaly
17.10758°
Mean motion
3.42587 °/min
Orbital period
105.08 mins
BSTAR
0.00010119
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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 | 2026-05-07 23:01:00.009Z | 350.526° N | 2026-05-07 23:07:00.009Z | 49.97° ENE | 44.92° | 2026-05-07 23:13:00.009Z | 169.721° S |
| 4 mins | 2026-05-08 00:51:00.009Z | 291.203° WNW | 2026-05-08 00:52:00.009Z | 281.446° WNW | 12.789° | 2026-05-08 00:55:00.009Z | 252.916° W |
| 8 mins | 2026-05-08 10:51:00.009Z | 125.627° SE | 2026-05-08 10:54:00.009Z | 91.688° ESE | 20.737° | 2026-05-08 10:59:00.009Z | 39.007° NE |
| 10 mins | 2026-05-08 12:36:00.009Z | 215.196° SW | 2026-05-08 12:40:00.009Z | 280.132° WNW | 38.581° | 2026-05-08 12:46:00.009Z | 0.17° NNE |
| 9 mins | 2026-05-08 21:50:00.009Z | 23.53° NE | 2026-05-08 21:54:00.009Z | 74.459° E | 24.848° | 2026-05-08 21:59:00.009Z | 126.032° SE |
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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