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: 19 hours ago
TLE from 19 hours ago
0 A-1 (ASTERIX)
1 01778U 65096A 26082.85212214 .00000274 00000-0 72401-4 0 9993
2 01778 34.2586 287.5242 0740201 316.2940 38.1339 13.49751163953253Epoch: 2026-03-23T20:27Z
TLE epoch observation values (Epoch: 2026-03-23T20:27:03.352Z)
Latitude
-0.00004°
Longitude
159.42199°
Altitude
655.371 km
Speed
7.739 km/s
True Right ascension
19h 10m 05s
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
20:07:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,628.085 km
Perigee altitude
524.528 km
Semi-major axis
7,454.443 km
Eccentricity
0.07402
Inclination
34.2586°
RAAN
287.5242°
Arg. of periapsis
316.294°
True anomaly
43.77209°
Mean anomaly
38.1339°
Eccentric anomaly
40.91131°
Mean motion
3.37225 °/min
Orbital period
106.75 mins
BSTAR
0.000072401
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-03-24 16:09:56.031Z | 183.947° SSW | 2026-03-24 16:13:56.031Z | 140.283° SSE | 19.205° | 2026-03-24 16:17:56.031Z | 105.427° ESE |
| 13 mins | 2026-03-24 18:00:56.031Z | 227.938° WSW | 2026-03-24 18:05:56.031Z | 161.634° S | 36.484° | 2026-03-24 18:13:56.031Z | 93.523° ESE |
| 15 mins | 2026-03-24 19:52:56.031Z | 255.296° W | 2026-03-24 19:58:56.031Z | 190.495° SSW | 40.965° | 2026-03-24 20:07:56.031Z | 105.938° ESE |
| 16 mins | 2026-03-24 21:45:56.031Z | 263.432° W | 2026-03-24 21:52:56.031Z | 198.521° SSW | 36.252° | 2026-03-24 22:01:56.031Z | 130.356° SE |
| 12 mins | 2026-03-24 23:40:56.031Z | 251.86° W | 2026-03-24 23:45:56.031Z | 215.995° SW | 22.334° | 2026-03-24 23:52:56.031Z | 168.718° 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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