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
Civil Science
Bus & Motor
ALOUETTE, Unknown motor
Mass
145 kg wet, 145 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Ell, 0.5 m
Radar Cross Section
0.784 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ALOUETTE 1 (S-27)
1 00424U 62049A 25242.94238127 .00000150 00000-0 16150-3 0 9994
2 00424 80.4689 183.5880 0021939 267.1083 92.7552 13.69526392141384Epoch: 2025-08-30T22:37Z
TLE epoch observation values (Epoch: 2025-08-30T22:37:01.741Z)
Latitude
-0.00003°
Longitude
-135.0387°
Altitude
1,004.904 km
Speed
7.349 km/s
True Right ascension
12h 14m 21s
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
20:03:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,014.722 km
Perigee altitude
982.355 km
Semi-major axis
7,376.675 km
Eccentricity
0.00219
Inclination
80.4689°
RAAN
183.588°
Arg. of periapsis
267.1083°
True anomaly
93.00628°
Mean anomaly
92.7552°
Eccentric anomaly
92.88074°
Mean motion
3.42572 °/min
Orbital period
105.09 mins
BSTAR
0.0001615
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Other satellites on launch #49 in the year 1962 (1962-09-29 UTC)
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 | 2025-08-31 06:13:40.911Z | 32.546° NE | 2025-08-31 06:16:40.911Z | 61.449° ENE | 14.044° | 2025-08-31 06:19:40.911Z | 90.65° ESE |
| 11 mins | 2025-08-31 07:58:40.911Z | 348.987° N | 2025-08-31 08:03:40.911Z | 324.239° NNW | 44.858° | 2025-08-31 08:09:40.911Z | 172.832° S |
| 8 mins | 2025-08-31 19:47:40.911Z | 128.034° SE | 2025-08-31 19:50:40.911Z | 92.944° ESE | 22.669° | 2025-08-31 19:55:40.911Z | 38.312° NE |
| 10 mins | 2025-08-31 21:32:40.911Z | 218.369° SW | 2025-08-31 21:36:40.911Z | 278.355° WNW | 37.074° | 2025-08-31 21:42:40.911Z | 358.34° 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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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Authenticating...
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