ALOUETTE 2, 1804
Orbit data source: Space-Track
ALOUETTE 2, 1804 is a payload satellite owned by DRTE (CA) in LEO that was launched on Mon, 29 Nov 1965 UTC via a THOR SLV-2 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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1804 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 + 1 Rod, 36.5 m
Radar Cross Section
0.732 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 ALOUETTE 2
1 01804U 65098A 25258.73609721 .00000848 00000-0 27238-3 0 9993
2 01804 79.8022 150.1016 1331630 68.8609 304.9393 12.27953985645581Epoch: 2025-09-15T17:39Z
TLE epoch observation values (Epoch: 2025-09-15T17:39:58.798Z)
Latitude
-0.00005°
Longitude
-109.82988°
Altitude
1,060.949 km
Speed
7.548 km/s
True Right ascension
10h 00m 24s
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
22:50:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,611.976 km
Perigee altitude
499.04 km
Semi-major axis
7,933.645 km
Eccentricity
0.13316
Inclination
79.8022°
RAAN
150.1016°
Arg. of periapsis
68.8609°
True anomaly
291.25123°
Mean anomaly
304.9393°
Eccentric anomaly
298.21626°
Mean motion
3.07138 °/min
Orbital period
117.21 mins
BSTAR
0.00027238
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Other satellites on launch #98 in the year 1965 (1965-11-29 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 2 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-16 17:14:10.040Z | 166.514° S | 2025-09-16 17:18:10.040Z | 105.194° ESE | 32.122° | 2025-09-16 17:21:10.040Z | 33.33° NE |
| 10 mins | 2025-09-17 03:27:10.040Z | 31.746° NE | 2025-09-17 03:30:10.040Z | 75.893° E | 26.968° | 2025-09-17 03:37:10.040Z | 134.492° SE |
| 11 mins | 2025-09-17 05:25:10.040Z | 316.031° NNW | 2025-09-17 05:29:10.040Z | 253.23° W | 31.751° | 2025-09-17 05:36:10.040Z | 200.065° SSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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