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
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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 ALOUETTE 2
1 01804U 65098A 25293.27659735 .00000753 00000-0 24615-3 0 9992
2 01804 79.7956 120.7418 1331311 358.9040 0.9174 12.28027437649829Epoch: 2025-10-20T06:38Z
TLE epoch observation values (Epoch: 2025-10-20T06:38:18.011Z)
Latitude
-0.00001°
Longitude
-7.81448°
Altitude
503.919 km
Speed
8.103 km/s
True Right ascension
08h 02m 58s
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
11:56:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,611.364 km
Perigee altitude
499.019 km
Semi-major axis
7,933.329 km
Eccentricity
0.13313
Inclination
79.7956°
RAAN
120.7418°
Arg. of periapsis
358.904°
True anomaly
1.20993°
Mean anomaly
0.9174°
Eccentric anomaly
1.05828°
Mean motion
3.07157 °/min
Orbital period
117.2 mins
BSTAR
0.00024615
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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. |
|---|---|---|---|---|---|---|---|
| 22 mins | 2025-10-20 22:47:39.813Z | 5.158° NNE | 2025-10-20 22:57:39.813Z | 71.869° E | 31.778° | 2025-10-20 23:09:39.813Z | 131.621° SE |
| 24 mins | 2025-10-21 00:46:39.813Z | 342.411° N | 2025-10-21 00:56:39.813Z | 262.144° W | 43.217° | 2025-10-21 01:10:39.813Z | 185.678° SSW |
| 13 mins | 2025-10-21 02:48:39.813Z | 307.714° NW | 2025-10-21 02:53:39.813Z | 281.659° WNW | 17.055° | 2025-10-21 03:01:39.813Z | 246.285° WSW |
| 8 mins | 2025-10-21 14:03:39.813Z | 232.891° WSW | 2025-10-21 14:05:39.813Z | 281.173° WNW | 34.192° | 2025-10-21 14:11:39.813Z | 1.307° NNE |
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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