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, 36.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ALOUETTE 2
1 01804U 65098A 26246.60194588 .00000468 00000-0 14563-3 0 9992
2 01804 79.7983 209.9368 1330814 73.5597 300.7265 12.28411132688900Epoch: 2026-09-03T14:26Z
TLE epoch observation values (Epoch: 2026-09-03T14:26:48.124Z)
Latitude
-0.00003°
Longitude
10.49851°
Altitude
1,133.451 km
Speed
7.479 km/s
True Right ascension
13h 59m 44s
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
11:54:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,609.097 km
Perigee altitude
497.98 km
Semi-major axis
7,931.675 km
Eccentricity
0.13308
Inclination
79.7983°
RAAN
209.9368°
Arg. of periapsis
73.5597°
True anomaly
286.55206°
Mean anomaly
300.7265°
Eccentric anomaly
293.74709°
Mean motion
3.07253 °/min
Orbital period
117.17 mins
BSTAR
0.00014563
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-09-03 22:22:14.274Z | 178.863° S | 2026-09-03 22:27:14.274Z | 68.54° E | 40.232° | 2026-09-03 22:30:14.274Z | 20.198° NNE |
| 10 mins | 2026-09-04 08:35:14.274Z | 25.011° NE | 2026-09-04 08:38:14.274Z | 77.781° E | 31.069° | 2026-09-04 08:45:14.274Z | 142.292° SSE |
| 10 mins | 2026-09-04 10:33:14.274Z | 310.032° NW | 2026-09-04 10:37:14.274Z | 255.395° W | 24.969° | 2026-09-04 10:43:14.274Z | 209.255° SW |
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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