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: 6 hours ago
TLE from 6 hours ago
0 A-1 (ASTERIX)
1 01778U 65096A 25342.57498940 .00001210 00000-0 31764-3 0 9999
2 01778 34.2603 76.9447 0740790 292.3937 59.9884 13.49658538939020Epoch: 2025-12-08T13:47Z
TLE epoch observation values (Epoch: 2025-12-08T13:47:59.084Z)
Latitude
-0.00003°
Longitude
152.37641°
Altitude
828.743 km
Speed
7.561 km/s
True Right ascension
05h 07m 46s
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
18:07:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,628.89 km
Perigee altitude
524.404 km
Semi-major axis
7,454.784 km
Eccentricity
0.07408
Inclination
34.2603°
RAAN
76.9447°
Arg. of periapsis
292.3937°
True anomaly
67.67211°
Mean anomaly
59.9884°
Eccentric anomaly
63.79663°
Mean motion
3.37202 °/min
Orbital period
106.76 mins
BSTAR
0.00031764
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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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2025-12-09 09:30:48.665Z | 207.582° SW | 2025-12-09 09:36:48.665Z | 149.978° SSE | 28.084° | 2025-12-09 09:43:48.665Z | 95.147° ESE |
| 16 mins | 2025-12-09 11:22:48.665Z | 241.702° WSW | 2025-12-09 11:29:48.665Z | 169.905° S | 40.061° | 2025-12-09 11:38:48.665Z | 95.149° ESE |
| 17 mins | 2025-12-09 13:15:48.665Z | 261.427° W | 2025-12-09 13:23:48.665Z | 185.041° SSW | 41.166° | 2025-12-09 13:32:48.665Z | 111.638° ESE |
| 16 mins | 2025-12-09 15:09:48.665Z | 265.019° W | 2025-12-09 15:17:48.665Z | 199.974° SSW | 33.603° | 2025-12-09 15:25:48.665Z | 140.581° SSE |
| 10 mins | 2025-12-09 17:05:48.665Z | 249.148° W | 2025-12-09 17:10:48.665Z | 216.588° SW | 17.148° | 2025-12-09 17:15:48.665Z | 183.97° SSW |
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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