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: 6 hours ago
TLE from 6 hours ago
0 ALOUETTE 2
1 1804U 65098A 26038.41705588 .00000424 00000-0 13251-3 0 9993
2 1804 79.7997 27.0467 1330998 135.6370 235.9482 12.28203787663342Epoch: 2026-02-07T10:00Z
TLE epoch observation values (Epoch: 2026-02-07T10:00:33.628Z)
Latitude
-0.00002°
Longitude
99.3657°
Altitude
2,237.362 km
Speed
6.506 km/s
True Right ascension
01h 48m 11s
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
17:53:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,610.255 km
Perigee altitude
498.608 km
Semi-major axis
7,932.569 km
Eccentricity
0.1331
Inclination
79.7997°
RAAN
27.0467°
Arg. of periapsis
135.637°
True anomaly
224.46768°
Mean anomaly
235.9482°
Eccentric anomaly
230.09793°
Mean motion
3.07201 °/min
Orbital period
117.19 mins
BSTAR
0.00013251
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-07 21:54:15.395Z | 108.656° ESE | 2026-02-07 21:57:15.395Z | 90.362° ESE | 12.973° | 2026-02-07 22:00:15.395Z | 68.825° E |
| 16 mins | 2026-02-07 23:46:15.395Z | 181.725° SSW | 2026-02-07 23:56:15.395Z | 78.772° E | 44.217° | 2026-02-08 00:02:15.395Z | 15.594° NNE |
| 10 mins | 2026-02-08 01:49:15.395Z | 251.348° W | 2026-02-08 01:54:15.395Z | 286.025° WNW | 19.593° | 2026-02-08 01:59:15.395Z | 331.901° NNW |
| 4 mins | 2026-02-08 10:07:15.395Z | 37.119° NE | 2026-02-08 10:09:15.395Z | 84.96° E | 19.966° | 2026-02-08 10:11:15.395Z | 121.064° SE |
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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