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
Civil Science
Bus & Motor
ALOUETTE, Unknown motor
Mass
145 kg wet, 145 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Ell + 1 Rod, 36.5 m
Radar Cross Section
0.732 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 ALOUETTE 2
1 01804U 65098A 25258.16581040 .00000934 00000-0 30095-3 0 9994
2 01804 79.8023 150.5861 1331633 70.0164 303.9131 12.27953630645517Epoch: 2025-09-15T03:58Z
TLE epoch observation values (Epoch: 2025-09-15T03:58:46.018Z)
Latitude
-0.00003°
Longitude
96.51998°
Altitude
1,078.823 km
Speed
7.531 km/s
True Right ascension
10h 02m 20s
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
10:17:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,611.98 km
Perigee altitude
499.039 km
Semi-major axis
7,933.646 km
Eccentricity
0.13316
Inclination
79.8023°
RAAN
150.5861°
Arg. of periapsis
70.0164°
True anomaly
290.09565°
Mean anomaly
303.9131°
Eccentric anomaly
297.12241°
Mean motion
3.07138 °/min
Orbital period
117.21 mins
BSTAR
0.00030095
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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 | 2025-09-15 17:46:27.038Z | 186.184° SSW | 2025-09-15 17:50:27.038Z | 160.11° S | 43.242° | 2025-09-15 17:54:27.038Z | 13.991° NNE |
| 12 mins | 2025-09-16 03:58:27.038Z | 10.397° NNE | 2025-09-16 04:02:27.038Z | 74.355° E | 35.668° | 2025-09-16 04:10:27.038Z | 149.119° SSE |
| 9 mins | 2025-09-16 05:58:27.038Z | 298.556° NW | 2025-09-16 06:01:27.038Z | 260.688° W | 22.738° | 2025-09-16 06:07:27.038Z | 215.194° SW |
| 6 mins | 2025-09-16 17:15:27.038Z | 159.337° S | 2025-09-16 17:18:27.038Z | 93.987° ESE | 32.16° | 2025-09-16 17:21:27.038Z | 31.092° NE |
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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