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: 1 day ago
TLE from 1 day ago
0 A-1 (ASTERIX)
1 01778U 65096A 26051.19132323 .00000206 00000-0 60781-4 0 9991
2 01778 34.2541 80.7299 0739281 92.6064 275.9353 13.49732455948970Epoch: 2026-02-20T04:35Z
TLE epoch observation values (Epoch: 2026-02-20T04:35:30.327Z)
Latitude
0°
Longitude
-138.27826°
Altitude
1,055.802 km
Speed
7.334 km/s
True Right ascension
05h 22m 55s
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
10:28:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,627.474 km
Perigee altitude
525.278 km
Semi-major axis
7,454.513 km
Eccentricity
0.07393
Inclination
34.2541°
RAAN
80.7299°
Arg. of periapsis
92.6064°
True anomaly
267.45897°
Mean anomaly
275.9353°
Eccentric anomaly
271.7014°
Mean motion
3.37221 °/min
Orbital period
106.76 mins
BSTAR
0.000060781
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-21 07:33:12.492Z | 245.339° WSW | 2026-02-21 07:37:12.492Z | 172.348° S | 30.469° | 2026-02-21 07:40:12.492Z | 113.159° SE |
| 5 mins | 2026-02-21 09:27:12.492Z | 237.448° WSW | 2026-02-21 09:29:12.492Z | 192.636° SSW | 24.121° | 2026-02-21 09:32:12.492Z | 137.887° SSE |
| 5 mins | 2026-02-22 04:46:12.492Z | 190.656° SSW | 2026-02-22 04:48:12.492Z | 161.596° S | 18.778° | 2026-02-22 04:51:12.492Z | 117.199° SE |
| 5 mins | 2026-02-22 06:38:12.492Z | 226.312° WSW | 2026-02-22 06:40:12.492Z | 184.898° SSW | 29.56° | 2026-02-22 06:43:12.492Z | 115.143° SE |
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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