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
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 ALOUETTE 2
1 01804U 65098A 26188.20211000 .00000591 00000-0 19135-3 0 9999
2 01804 79.7983 259.6224 1330477 191.9297 164.7128 12.28368520681732Epoch: 2026-07-07T04:51Z
TLE epoch observation values (Epoch: 2026-07-07T04:51:02.303Z)
Latitude
-0.00007°
Longitude
-98.31333°
Altitude
2,585.555 km
Speed
6.223 km/s
True Right ascension
17h 18m 29s
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
06:19:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,609.038 km
Perigee altitude
498.406 km
Semi-major axis
7,931.859 km
Eccentricity
0.13305
Inclination
79.7983°
RAAN
259.6224°
Arg. of periapsis
191.9297°
True anomaly
168.17241°
Mean anomaly
164.7128°
Eccentric anomaly
166.49324°
Mean motion
3.07242 °/min
Orbital period
117.17 mins
BSTAR
0.00019135
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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. |
|---|---|---|---|---|---|---|---|
| 24 mins | 2026-07-08 04:21:44.200Z | 155.754° SSE | 2026-07-08 04:34:44.200Z | 92.915° ESE | 36.205° | 2026-07-08 04:45:44.200Z | 24.147° NE |
| 24 mins | 2026-07-08 06:20:44.200Z | 209.948° SW | 2026-07-08 06:33:44.200Z | 287.593° WNW | 40.66° | 2026-07-08 06:44:44.200Z | 3.272° NNE |
| 12 mins | 2026-07-08 08:28:44.200Z | 277.826° WNW | 2026-07-08 08:34:44.200Z | 305.793° NW | 15.497° | 2026-07-08 08:40:44.200Z | 337.313° NNW |
| 4 mins | 2026-07-08 14:50:44.200Z | 35.972° NE | 2026-07-08 14:51:44.200Z | 46.13° ENE | 13.455° | 2026-07-08 14:54:44.200Z | 80.56° E |
| 8 mins | 2026-07-08 16:47:44.200Z | 339.663° N | 2026-07-08 16:52:44.200Z | 239.075° WSW | 39.777° | 2026-07-08 16:55:44.200Z | 188.783° 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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