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: 23 hours ago
TLE from 23 hours ago
0 A-1 (ASTERIX)
1 01778U 65096A 25323.85864418 .00000835 00000-0 22231-3 0 9997
2 01778 34.2532 167.5018 0740097 160.2069 202.8950 13.49618102936495Epoch: 2025-11-19T20:36Z
TLE epoch observation values (Epoch: 2025-11-19T20:36:26.857Z)
Latitude
-0.00002°
Longitude
159.26552°
Altitude
1,586.131 km
Speed
6.83 km/s
True Right ascension
11h 10m 00s
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
16:26:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,628.534 km
Perigee altitude
525.059 km
Semi-major axis
7,454.934 km
Eccentricity
0.07401
Inclination
34.2532°
RAAN
167.5018°
Arg. of periapsis
160.2069°
True anomaly
199.8568°
Mean anomaly
202.895°
Eccentric anomaly
201.35113°
Mean motion
3.37192 °/min
Orbital period
106.76 mins
BSTAR
0.00022231
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-11-20 20:04:04.559Z | 257.873° W | 2025-11-20 20:11:04.559Z | 169.956° S | 36.758° | 2025-11-20 20:15:04.559Z | 113.789° SE |
| 6 mins | 2025-11-20 22:00:04.559Z | 247.197° WSW | 2025-11-20 22:03:04.559Z | 200.815° SSW | 24.387° | 2025-11-20 22:06:04.559Z | 152.178° SSE |
| 11 mins | 2025-11-21 15:22:04.559Z | 190.023° SSW | 2025-11-21 15:27:04.559Z | 155.432° SSE | 19.934° | 2025-11-21 15:33:04.559Z | 107.286° ESE |
| 12 mins | 2025-11-21 17:14:04.559Z | 226.231° WSW | 2025-11-21 17:21:04.559Z | 157.814° S | 33.34° | 2025-11-21 17:26:04.559Z | 101.272° ESE |
| 11 mins | 2025-11-21 19:08:04.559Z | 250.448° W | 2025-11-21 19:14:04.559Z | 172.177° S | 38.512° | 2025-11-21 19:19:04.559Z | 106.191° 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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