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: 13 hours ago
TLE from 13 hours ago
0 ALOUETTE 1 (S-27)
1 424U 62049A 26196.16635595 .00000064 00000-0 63143-4 0 9996
2 424 80.4645 228.6980 0023418 162.1589 198.0384 13.69595190184941Epoch: 2026-07-15T03:59Z
TLE epoch observation values (Epoch: 2026-07-15T03:59:33.154Z)
Latitude
-0.00003°
Longitude
-124.21621°
Altitude
1,020.281 km
Speed
7.333 km/s
True Right ascension
15h 14m 47s
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
05:05:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,015.566 km
Perigee altitude
981.017 km
Semi-major axis
7,376.428 km
Eccentricity
0.00234
Inclination
80.4645°
RAAN
228.698°
Arg. of periapsis
162.1589°
True anomaly
197.95553°
Mean anomaly
198.0384°
Eccentric anomaly
197.99694°
Mean motion
3.42589 °/min
Orbital period
105.08 mins
BSTAR
0.000063143
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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 | 2026-07-16 02:53:03.686Z | 182.341° SSW | 2026-07-16 02:59:03.686Z | 79.056° E | 44.277° | 2026-07-16 03:05:03.686Z | 13.364° NNE |
| 6 mins | 2026-07-16 04:43:03.686Z | 267.342° W | 2026-07-16 04:46:03.686Z | 298.417° NW | 15.785° | 2026-07-16 04:49:03.686Z | 328.632° NNW |
| 4 mins | 2026-07-16 12:10:03.686Z | 44.241° NE | 2026-07-16 12:12:03.686Z | 64.364° ENE | 12.885° | 2026-07-16 12:14:03.686Z | 83.958° E |
| 11 mins | 2026-07-16 13:54:03.686Z | 350.178° N | 2026-07-16 13:59:03.686Z | 146.535° SSE | 44.97° | 2026-07-16 14:05:03.686Z | 171.047° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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