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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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 26101.27597640 .00000186 00000-0 55611-4 0 9996
2 01778 34.2534 198.3623 0739421 86.5191 281.9667 13.49762454955748Epoch: 2026-04-11T06:37Z
TLE epoch observation values (Epoch: 2026-04-11T06:37:24.360Z)
Latitude
-0.00006°
Longitude
-100.4869°
Altitude
997.577 km
Speed
7.391 km/s
True Right ascension
13h 13m 26s
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
18:31:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,627.46 km
Perigee altitude
525.071 km
Semi-major axis
7,454.403 km
Eccentricity
0.07394
Inclination
34.2534°
RAAN
198.3623°
Arg. of periapsis
86.5191°
True anomaly
273.54635°
Mean anomaly
281.9667°
Eccentric anomaly
277.76902°
Mean motion
3.37228 °/min
Orbital period
106.75 mins
BSTAR
0.000055611
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-04-11 12:16:14.075Z | 240.043° WSW | 2026-04-11 12:19:14.075Z | 186.427° SSW | 29.366° | 2026-04-11 12:22:14.075Z | 115.5° SE |
| 5 mins | 2026-04-11 14:10:14.075Z | 228.049° WSW | 2026-04-11 14:11:14.075Z | 203.869° SW | 25.472° | 2026-04-11 14:15:14.075Z | 130.686° SE |
| 4 mins | 2026-04-12 09:29:14.075Z | 182.521° SSW | 2026-04-12 09:31:14.075Z | 152.53° SSE | 15.287° | 2026-04-12 09:33:14.075Z | 123.315° SE |
| 6 mins | 2026-04-12 11:20:14.075Z | 228.051° WSW | 2026-04-12 11:23:14.075Z | 164.545° S | 27.76° | 2026-04-12 11:26:14.075Z | 109.489° ESE |
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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