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: 1 day ago
TLE from 1 day ago
0 ALOUETTE 2
1 01804U 65098A 26247.33490210 .00000462 00000-0 14350-3 0 9992
2 01804 79.7984 209.3134 1330809 72.0732 302.0658 12.28411801688998Epoch: 2026-09-04T08:02Z
TLE epoch observation values (Epoch: 2026-09-04T08:02:15.541Z)
Latitude
0.00007°
Longitude
105.28845°
Altitude
1,109.666 km
Speed
7.501 km/s
True Right ascension
13h 57m 15s
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
09:25:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,609.09 km
Perigee altitude
497.981 km
Semi-major axis
7,931.672 km
Eccentricity
0.13308
Inclination
79.7984°
RAAN
209.3134°
Arg. of periapsis
72.0732°
True anomaly
288.03881°
Mean anomaly
302.0658°
Eccentric anomaly
295.16451°
Mean motion
3.07253 °/min
Orbital period
117.17 mins
BSTAR
0.0001435
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-05 21:18:00.995Z | 133.374° SE | 2026-09-05 21:21:00.995Z | 90.692° ESE | 15.628° | 2026-09-05 21:23:00.995Z | 58.216° ENE |
| 5 mins | 2026-09-05 23:17:00.995Z | 246.526° WSW | 2026-09-05 23:19:00.995Z | 283.17° WNW | 20.932° | 2026-09-05 23:22:00.995Z | 338.334° N |
| 6 mins | 2026-09-06 07:30:00.995Z | 48.02° ENE | 2026-09-06 07:32:00.995Z | 69.956° E | 14.909° | 2026-09-06 07:36:00.995Z | 104.375° ESE |
| 12 mins | 2026-09-06 09:27:00.995Z | 338.052° N | 2026-09-06 09:31:00.995Z | 237.03° WSW | 42.875° | 2026-09-06 09:39:00.995Z | 179.822° S |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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