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
Civil Technology
Bus & Motor
A-1, Unknown motor
Mass
42 kg wet, 42 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Poly, 0.3 m
Radar Cross Section
0.337 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 A-1 (ASTERIX)
1 01778U 65096A 25259.04198379 .00000783 00000-0 21555-3 0 9992
2 01778 34.2536 121.0479 0740312 62.2773 305.0985 13.49412600927734Epoch: 2025-09-16T01:00Z
TLE epoch observation values (Epoch: 2025-09-16T01:00:27.399Z)
Latitude
-0.00002°
Longitude
110.69574°
Altitude
785.257 km
Speed
7.606 km/s
True Right ascension
08h 04m 11s
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
20:22:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,629.507 km
Perigee altitude
525.599 km
Semi-major axis
7,455.69 km
Eccentricity
0.07403
Inclination
34.2536°
RAAN
121.0479°
Arg. of periapsis
62.2773°
True anomaly
297.7886°
Mean anomaly
305.0985°
Eccentric anomaly
301.48115°
Mean motion
3.37141 °/min
Orbital period
106.78 mins
BSTAR
0.00021555
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-17 18:05:47.401Z | 189.369° SSW | 2025-09-17 18:07:47.401Z | 154.809° SSE | 15.973° | 2025-09-17 18:09:47.401Z | 121.894° SE |
| 5 mins | 2025-09-17 19:57:47.401Z | 222.198° SW | 2025-09-17 19:59:47.401Z | 167.461° S | 29.047° | 2025-09-17 20:02:47.401Z | 110.758° ESE |
| 6 mins | 2025-09-17 21:49:47.401Z | 237.718° WSW | 2025-09-17 21:51:47.401Z | 190.229° SSW | 28.376° | 2025-09-17 21:55:47.401Z | 125.582° SE |
| 4 mins | 2025-09-17 23:42:47.401Z | 221.522° SW | 2025-09-17 23:43:47.401Z | 206.523° SW | 16.074° | 2025-09-17 23:46:47.401Z | 167.775° 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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