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: 10 hours ago
TLE from 10 hours ago
0 A-1 (ASTERIX)
1 1778U 65096A 25298.40519600 .00001699 00000-0 45251-3 0 9995
2 1778 34.2582 290.6485 0740673 340.3137 17.0277 13.49551016933050Epoch: 2025-10-25T09:43Z
TLE epoch observation values (Epoch: 2025-10-25T09:43:28.934Z)
Latitude
-0.00005°
Longitude
110.74165°
Altitude
549.099 km
Speed
7.851 km/s
True Right ascension
19h 22m 35s
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
14:56:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,629.228 km
Perigee altitude
524.858 km
Semi-major axis
7,455.18 km
Eccentricity
0.07407
Inclination
34.2582°
RAAN
290.6485°
Arg. of periapsis
340.3137°
True anomaly
19.75243°
Mean anomaly
17.0277°
Eccentric anomaly
18.36476°
Mean motion
3.37175 °/min
Orbital period
106.77 mins
BSTAR
0.00045251
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-10-26 03:43:50.711Z | 212.21° SW | 2025-10-26 03:46:50.711Z | 166.891° S | 30.602° | 2025-10-26 03:53:50.711Z | 94.733° ESE |
| 13 mins | 2025-10-26 05:34:50.711Z | 249.809° W | 2025-10-26 05:39:50.711Z | 184.185° SSW | 39.772° | 2025-10-26 05:47:50.711Z | 102.652° ESE |
| 14 mins | 2025-10-26 07:27:50.711Z | 259.251° W | 2025-10-26 07:33:50.711Z | 185.974° SSW | 36.798° | 2025-10-26 07:41:50.711Z | 124.718° SE |
| 13 mins | 2025-10-26 09:20:50.711Z | 256.189° W | 2025-10-26 09:26:50.711Z | 207.947° SW | 24.788° | 2025-10-26 09:33:50.711Z | 159.285° S |
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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