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: 17 hours ago
TLE from 17 hours ago
0 A-1 (ASTERIX)
1 01778U 65096A 25310.09771404 .00001140 00000-0 30967-3 0 9996
2 01778 34.2542 234.0810 0740084 62.9403 304.4814 13.49582800934639Epoch: 2025-11-06T02:20Z
TLE epoch observation values (Epoch: 2025-11-06T02:20:42.493Z)
Latitude
-0.00002°
Longitude
153.343°
Altitude
790.018 km
Speed
7.601 km/s
True Right ascension
15h 36m 19s
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
15:43:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,628.664 km
Perigee altitude
525.189 km
Semi-major axis
7,455.064 km
Eccentricity
0.07401
Inclination
34.2542°
RAAN
234.081°
Arg. of periapsis
62.9403°
True anomaly
297.12557°
Mean anomaly
304.4814°
Eccentric anomaly
300.84063°
Mean motion
3.37183 °/min
Orbital period
106.77 mins
BSTAR
0.00030967
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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 | 2025-11-06 23:57:31.486Z | 211.512° SW | 2025-11-06 23:59:31.486Z | 159.495° S | 26.14° | 2025-11-07 00:02:31.486Z | 108.267° ESE |
| 6 mins | 2025-11-07 01:49:31.486Z | 234.482° WSW | 2025-11-07 01:51:31.486Z | 180.17° SSW | 30.809° | 2025-11-07 01:55:31.486Z | 117.488° SE |
| 6 mins | 2025-11-07 03:41:31.486Z | 234.745° WSW | 2025-11-07 03:43:31.486Z | 201.389° SSW | 20.816° | 2025-11-07 03:47:31.486Z | 149.605° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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