Showing default

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.

Loading next visibility...
Identifier
1804, 1965-098A
Orbit
LEO
Country
Flag of CACA
Related business
Manufacturer
DEHAVT/RCAV
Mission
Spacecraft
Bus & Motor
ALOUETTE, Unknown motor
Mass
145 kg wet, 145 kg dry
Launch date (UTC)
1965-11-29 (60 years ago)
Launch vehicle
THOR SLV-2 AGENA B
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 ALOUETTE 2
1 01804U 65098A   26125.97430331  .00000221  00000-0  73531-4 0  9995
2 01804  79.7988 312.5888 1330409 318.1635  32.4812 12.28317958674097
Epoch: 2026-05-05T23:22Z
TLE epoch observation values (Epoch: 2026-05-05T23:22:59.805Z)
Latitude
-0.00011°
Longitude
97.99814°
Altitude
716.896 km
Speed
7.885 km/s
True Right ascension
20h 50m 21s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
02:15:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,609.23 km
Perigee altitude
498.649 km
Semi-major axis
7,932.077 km
Eccentricity
0.13304
Inclination
79.7988°
RAAN
312.5888°
Arg. of periapsis
318.1635°
True anomaly
41.94992°
Mean anomaly
32.4812°
Eccentric anomaly
37.0768°
Mean motion
3.07229 °/min
Orbital period
117.18 mins
BSTAR
0.000073531
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|