A-1 (ASTERIX), 1778
Orbit data source: Space-Track
A-1 (ASTERIX), 1778 is a payload satellite owned by CNES (FR) in LEO that was launched on Fri, 26 Nov 1965 UTC via a DIAMANT A launch vehicle from the Hamma Guira Space Track Range (HGSTR). 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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1778 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
FRRelated business
Manufacturer
CNES
Mission
Spacecraft
Bus & Motor
A-1, Unknown motor
Mass
42 kg wet, 42 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: 1 day ago
TLE from 1 day ago
0 A-1 (ASTERIX)
1 01778U 65096A 25311.79961010 .00001294 00000-0 35029-3 0 9992
2 01778 34.2539 225.8470 0740041 74.9688 293.1608 13.49588103934868Epoch: 2025-11-07T19:11Z
TLE epoch observation values (Epoch: 2025-11-07T19:11:26.312Z)
Latitude
-0.00002°
Longitude
-109.25105°
Altitude
891.757 km
Speed
7.497 km/s
True Right ascension
15h 03m 23s
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
16:44:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,628.611 km
Perigee altitude
525.203 km
Semi-major axis
7,455.044 km
Eccentricity
0.074
Inclination
34.2539°
RAAN
225.847°
Arg. of periapsis
74.9688°
True anomaly
285.09692°
Mean anomaly
293.1608°
Eccentric anomaly
289.15545°
Mean motion
3.37185 °/min
Orbital period
106.77 mins
BSTAR
0.00035029
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Other satellites on launch #96 in the year 1965 (1965-11-26 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.A-1 (ASTERIX) 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 | 2025-11-08 22:03:37.338Z | 207.829° SW | 2025-11-08 22:06:37.338Z | 161.512° S | 18.513° | 2025-11-08 22:08:37.338Z | 124.805° SE |
| 5 mins | 2025-11-08 23:56:37.338Z | 229.372° WSW | 2025-11-08 23:58:37.338Z | 179.557° S | 29.743° | 2025-11-09 00:01:37.338Z | 114.007° SE |
| 6 mins | 2025-11-09 01:48:37.338Z | 241.009° WSW | 2025-11-09 01:50:37.338Z | 198.988° SSW | 25.997° | 2025-11-09 01:54:37.338Z | 130.393° SE |
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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