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
POLY, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 A-1 (ASTERIX)
1 01778U 65096A 26262.91179715 .00000338 00000-0 91384-4 0 9990
2 01778 34.2536 136.0706 0738873 148.9640 215.6890 13.49921758977596Epoch: 2026-09-19T21:52Z
TLE epoch observation values (Epoch: 2026-09-19T21:52:59.273Z)
Latitude
-0.00001°
Longitude
169.01008°
Altitude
1,531.174 km
Speed
6.88 km/s
True Right ascension
09h 04m 16s
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
06:48:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,626.422 km
Perigee altitude
524.937 km
Semi-major axis
7,453.817 km
Eccentricity
0.07389
Inclination
34.2536°
RAAN
136.0706°
Arg. of periapsis
148.964°
True anomaly
211.09995°
Mean anomaly
215.689°
Eccentric anomaly
213.36099°
Mean motion
3.37268 °/min
Orbital period
106.74 mins
BSTAR
0.000091384
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-09-20 17:33:12.209Z | 187.464° SSW | 2026-09-20 17:38:12.209Z | 151.164° SSE | 17.708° | 2026-09-20 17:42:12.209Z | 116.749° SE |
| 11 mins | 2026-09-20 19:25:12.209Z | 222.952° SW | 2026-09-20 19:31:12.209Z | 162.032° S | 36.371° | 2026-09-20 19:36:12.209Z | 101.458° ESE |
| 9 mins | 2026-09-20 21:19:12.209Z | 246.896° WSW | 2026-09-20 21:24:12.209Z | 169.558° S | 48.622° | 2026-09-20 21:28:12.209Z | 107.976° ESE |
| 7 mins | 2026-09-20 23:13:12.209Z | 250.432° W | 2026-09-20 23:16:12.209Z | 200.918° SSW | 34.41° | 2026-09-20 23:20:12.209Z | 132.551° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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