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: 18 hours ago
TLE from 18 hours ago
0 ALOUETTE 2
1 01804U 65098A 26292.12351907 .00000552 00000-0 17941-3 0 9997
2 01804 79.8002 171.2201 1330806 341.2828 14.3399 12.28467121694499Epoch: 2026-10-19T02:57Z
TLE epoch observation values (Epoch: 2026-10-19T02:57:52.047Z)
Latitude
-0.00006°
Longitude
99.14724°
Altitude
546.063 km
Speed
8.059 km/s
True Right ascension
11h 24m 52s
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
15:45:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,608.817 km
Perigee altitude
497.777 km
Semi-major axis
7,931.434 km
Eccentricity
0.13308
Inclination
79.8002°
RAAN
171.2201°
Arg. of periapsis
341.2828°
True anomaly
18.83108°
Mean anomaly
14.3399°
Eccentric anomaly
16.50631°
Mean motion
3.07267 °/min
Orbital period
117.16 mins
BSTAR
0.00017941
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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. |
|---|---|---|---|---|---|---|---|
| 16 mins | 2026-10-20 01:00:38.257Z | 16.558° NNE | 2026-10-20 01:08:38.257Z | 56.818° ENE | 18.571° | 2026-10-20 01:16:38.257Z | 91.575° ESE |
| 25 mins | 2026-10-20 02:58:38.257Z | 357.542° N | 2026-10-20 03:09:38.257Z | 78.685° E | 62.863° | 2026-10-20 03:23:38.257Z | 153.834° SSE |
| 23 mins | 2026-10-20 04:57:38.257Z | 333.308° NNW | 2026-10-20 05:07:38.257Z | 273.757° WNW | 45.691° | 2026-10-20 05:20:38.257Z | 207.566° SW |
| 9 mins | 2026-10-20 16:13:38.257Z | 143.478° SSE | 2026-10-20 16:16:38.257Z | 83.365° E | 41.377° | 2026-10-20 16:22:38.257Z | 23.669° NE |
| 9 mins | 2026-10-20 18:12:38.257Z | 262.253° W | 2026-10-20 18:15:38.257Z | 302.299° NW | 24.82° | 2026-10-20 18:21:38.257Z | 353.052° N |
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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