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: 17 hours ago
TLE from 17 hours ago
0 ALOUETTE 2
1 01804U 65098A 26186.16569030 .00000900 00000-0 29302-3 0 9992
2 01804 79.7988 261.3551 1330386 196.0585 159.4133 12.28367021681489Epoch: 2026-07-05T03:58Z
TLE epoch observation values (Epoch: 2026-07-05T03:58:35.641Z)
Latitude
-0.00007°
Longitude
-81.46235°
Altitude
2,561.834 km
Speed
6.242 km/s
True Right ascension
17h 25m 25s
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
08:57:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,608.973 km
Perigee altitude
498.484 km
Semi-major axis
7,931.865 km
Eccentricity
0.13304
Inclination
79.7988°
RAAN
261.3551°
Arg. of periapsis
196.0585°
True anomaly
164.04378°
Mean anomaly
159.4133°
Eccentric anomaly
161.79475°
Mean motion
3.07242 °/min
Orbital period
117.17 mins
BSTAR
0.00029302
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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. |
|---|---|---|---|---|---|---|---|
| 17 mins | 2026-07-06 03:33:29.198Z | 120.891° SE | 2026-07-06 03:42:29.198Z | 82.433° E | 20.348° | 2026-07-06 03:50:29.198Z | 41.938° NE |
| 26 mins | 2026-07-06 05:26:29.198Z | 178.135° S | 2026-07-06 05:40:29.198Z | 87.253° E | 44.224° | 2026-07-06 05:52:29.198Z | 14.434° NNE |
| 22 mins | 2026-07-06 07:28:29.198Z | 235.527° WSW | 2026-07-06 07:39:29.198Z | 291.083° WNW | 30.527° | 2026-07-06 07:50:29.198Z | 356.427° N |
| 9 mins | 2026-07-06 15:54:29.198Z | 6.068° NNE | 2026-07-06 15:59:29.198Z | 67.031° ENE | 30.273° | 2026-07-06 16:03:29.198Z | 130.578° SE |
| 6 mins | 2026-07-06 17:54:29.198Z | 313.419° NW | 2026-07-06 17:57:29.198Z | 277.196° WNW | 19.702° | 2026-07-06 18:00:29.198Z | 234.972° WSW |
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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