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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Edit Public Description
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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ALOUETTE 2
1 1804U 65098A 25290.09966150 .00000740 00000-0 24134-3 0 9993
2 1804 79.7957 123.4435 1331410 5.3401 356.0363 12.28023066649439Epoch: 2025-10-17T02:23Z
TLE epoch observation values (Epoch: 2025-10-17T02:23:30.753Z)
Latitude
0.00001°
Longitude
61.71547°
Altitude
507.022 km
Speed
8.1 km/s
True Right ascension
08h 13m 46s
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
03:11:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,611.464 km
Perigee altitude
498.957 km
Semi-major axis
7,933.347 km
Eccentricity
0.13314
Inclination
79.7957°
RAAN
123.4435°
Arg. of periapsis
5.3401°
True anomaly
354.77389°
Mean anomaly
356.0363°
Eccentric anomaly
355.42826°
Mean motion
3.07156 °/min
Orbital period
117.2 mins
BSTAR
0.00024134
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-10-17 14:13:58.342Z | 204.073° SW | 2025-10-17 14:17:58.342Z | 305.517° NW | 40.766° | 2025-10-17 14:22:58.342Z | 5.828° NNE |
| 15 mins | 2025-10-17 22:28:58.342Z | 23.47° NE | 2025-10-17 22:34:58.342Z | 61.423° ENE | 20.916° | 2025-10-17 22:43:58.342Z | 106.059° ESE |
| 23 mins | 2025-10-18 00:25:58.342Z | 352.59° N | 2025-10-18 00:34:58.342Z | 76.333° E | 44.532° | 2025-10-18 00:48:58.342Z | 166.457° S |
| 18 mins | 2025-10-18 02:25:58.342Z | 319.975° NNW | 2025-10-18 02:32:58.342Z | 275.098° WNW | 27.133° | 2025-10-18 02:43:58.342Z | 221.666° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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