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 25356.33853308 .00000442 00000-0 12315-3 0 9998
2 01778 34.2568 10.3512 0739842 29.6221 334.4315 13.49675666940885Epoch: 2025-12-22T08:07Z
TLE epoch observation values (Epoch: 2025-12-22T08:07:29.258Z)
Latitude
-0°
Longitude
157.34123°
Altitude
583.563 km
Speed
7.814 km/s
True Right ascension
00h 41m 24s
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
05:49:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,628.116 km
Perigee altitude
525.053 km
Semi-major axis
7,454.721 km
Eccentricity
0.07398
Inclination
34.2568°
RAAN
10.3512°
Arg. of periapsis
29.6221°
True anomaly
330.44407°
Mean anomaly
334.4315°
Eccentric anomaly
332.47234°
Mean motion
3.37207 °/min
Orbital period
106.76 mins
BSTAR
0.00012315
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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 | 2025-12-23 07:32:50.275Z | 252.663° W | 2025-12-23 07:36:50.275Z | 193.471° SSW | 34.979° | 2025-12-23 07:42:50.275Z | 109.952° ESE |
| 9 mins | 2025-12-23 09:26:50.275Z | 243.487° WSW | 2025-12-23 09:29:50.275Z | 196.197° SSW | 28.594° | 2025-12-23 09:35:50.275Z | 135.997° SSE |
| 6 mins | 2025-12-23 11:20:50.275Z | 224.884° SW | 2025-12-23 11:22:50.275Z | 206.161° SW | 15.01° | 2025-12-23 11:26:50.275Z | 175.617° S |
| 5 mins | 2025-12-24 04:46:50.275Z | 193.523° SSW | 2025-12-24 04:48:50.275Z | 151.396° SSE | 21.027° | 2025-12-24 04:51:50.275Z | 107.758° ESE |
| 4 mins | 2025-12-24 06:37:50.275Z | 238.281° WSW | 2025-12-24 06:40:50.275Z | 167.669° S | 33.746° | 2025-12-24 06:41:50.275Z | 138.943° SSE |
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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