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: 6 hours ago
TLE from 6 hours ago
0 A-1 (ASTERIX)
1 1778U 65096A 26177.69193837 .00000498 00000-0 12838-3 0 9994
2 1778 34.2576 188.5498 0739712 266.5793 85.0044 13.49824580966075Epoch: 2026-06-26T16:36Z
TLE epoch observation values (Epoch: 2026-06-26T16:36:23.475Z)
Latitude
0.00002°
Longitude
24.63521°
Altitude
1,064.525 km
Speed
7.325 km/s
True Right ascension
12h 34m 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
10:01:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,627.431 km
Perigee altitude
524.642 km
Semi-major axis
7,454.174 km
Eccentricity
0.07397
Inclination
34.2576°
RAAN
188.5498°
Arg. of periapsis
266.5793°
True anomaly
93.48609°
Mean anomaly
85.0044°
Eccentric anomaly
89.24227°
Mean motion
3.37244 °/min
Orbital period
106.75 mins
BSTAR
0.00012838
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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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2026-06-27 03:24:38.466Z | 202.218° SSW | 2026-06-27 03:31:38.466Z | 147.651° SSE | 25.916° | 2026-06-27 03:39:38.466Z | 93.665° ESE |
| 17 mins | 2026-06-27 05:17:38.466Z | 233.965° WSW | 2026-06-27 05:24:38.466Z | 168.968° S | 39.04° | 2026-06-27 05:34:38.466Z | 91.882° ESE |
| 17 mins | 2026-06-27 07:10:38.466Z | 258.021° W | 2026-06-27 07:18:38.466Z | 188.035° SSW | 41.787° | 2026-06-27 07:27:38.466Z | 106.35° ESE |
| 16 mins | 2026-06-27 09:04:38.466Z | 266.054° W | 2026-06-27 09:12:38.466Z | 201.151° SSW | 36.323° | 2026-06-27 09:20:38.466Z | 132.866° SE |
| 10 mins | 2026-06-27 11:00:38.466Z | 252.593° W | 2026-06-27 11:05:38.466Z | 216.34° SW | 20.325° | 2026-06-27 11:10:38.466Z | 177.54° 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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