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
ELL + ANT, 1.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ALOUETTE 2
1 1804U 65098A 26306.53688080 .00000223 00000-0 73984-4 0 9998
2 1804 79.7983 158.9540 1330253 312.0514 37.4540 12.28476615696267Epoch: 2026-11-02T12:53Z
TLE epoch observation values (Epoch: 2026-11-02T12:53:06.501Z)
Latitude
-0.00008°
Longitude
-76.13558°
Altitude
781.728 km
Speed
7.82 km/s
True Right ascension
10h 35m 48s
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
18:07:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,608.332 km
Perigee altitude
498.18 km
Semi-major axis
7,931.393 km
Eccentricity
0.13303
Inclination
79.7983°
RAAN
158.954°
Arg. of periapsis
312.0514°
True anomaly
48.06179°
Mean anomaly
37.454°
Eccentric anomaly
42.61442°
Mean motion
3.07269 °/min
Orbital period
117.16 mins
BSTAR
0.000073984
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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. |
|---|---|---|---|---|---|---|---|
| 18 mins | 2026-11-02 23:14:04.913Z | 8.463° NNE | 2026-11-02 23:23:04.913Z | 48.566° ENE | 20.053° | 2026-11-02 23:32:04.913Z | 88.443° E |
| 27 mins | 2026-11-03 01:12:04.913Z | 354.336° N | 2026-11-03 01:25:04.913Z | 65.929° ENE | 62.489° | 2026-11-03 01:39:04.913Z | 152.525° SSE |
| 24 mins | 2026-11-03 03:12:04.913Z | 336.512° NNW | 2026-11-03 03:24:04.913Z | 271.788° WNW | 46.84° | 2026-11-03 03:36:04.913Z | 207.776° SW |
| 15 mins | 2026-11-03 14:24:04.913Z | 153.837° SSE | 2026-11-03 14:29:04.913Z | 91.408° ESE | 47.92° | 2026-11-03 14:39:04.913Z | 19.33° NNE |
| 15 mins | 2026-11-03 16:23:04.913Z | 242.093° WSW | 2026-11-03 16:28:04.913Z | 295.168° NW | 36.06° | 2026-11-03 16:38:04.913Z | 1.364° NNE |
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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