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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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: 13 hours ago
TLE from 13 hours ago
0 ALOUETTE 2
1 01804U 65098A 26072.30316283 .00001090 00000-0 35077-3 0 9999
2 01804 79.8058 358.2401 1330834 66.9449 306.6225 12.28248577667509Epoch: 2026-03-13T07:16Z
TLE epoch observation values (Epoch: 2026-03-13T07:16:33.268Z)
Latitude
-0.00005°
Longitude
78.16084°
Altitude
1,031.003 km
Speed
7.577 km/s
True Right ascension
23h 52m 57s
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
00:21:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,609.906 km
Perigee altitude
498.571 km
Semi-major axis
7,932.375 km
Eccentricity
0.13308
Inclination
79.8058°
RAAN
358.2401°
Arg. of periapsis
66.9449°
True anomaly
293.16736°
Mean anomaly
306.6225°
Eccentric anomaly
300.02031°
Mean motion
3.07212 °/min
Orbital period
117.18 mins
BSTAR
0.00035077
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-13 21:06:55.580Z | 254.898° W | 2026-03-13 21:08:55.580Z | 285.026° WNW | 14.151° | 2026-03-13 21:10:55.580Z | 319.351° NNW |
| 8 mins | 2026-03-14 05:19:55.580Z | 43.853° NE | 2026-03-14 05:21:55.580Z | 68.737° E | 20.459° | 2026-03-14 05:27:55.580Z | 120.06° SE |
| 12 mins | 2026-03-14 07:16:55.580Z | 329.019° NNW | 2026-03-14 07:20:55.580Z | 256.55° W | 38.931° | 2026-03-14 07:28:55.580Z | 188.868° SSW |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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