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: 15 hours ago
TLE from 15 hours ago
0 A-1 (ASTERIX)
1 01778U 65096A 26141.66712272 .00000265 00000-0 75212-4 0 9990
2 01778 34.2576 2.8946 0739244 11.9169 349.7988 13.49780587961205Epoch: 2026-05-21T16:00Z
TLE epoch observation values (Epoch: 2026-05-21T16:00:39.403Z)
Latitude
-0.00002°
Longitude
-116.57864°
Altitude
531.395 km
Speed
7.869 km/s
True Right ascension
00h 11m 34s
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
15:39:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,627.256 km
Perigee altitude
525.141 km
Semi-major axis
7,454.335 km
Eccentricity
0.07392
Inclination
34.2576°
RAAN
2.8946°
Arg. of periapsis
11.9169°
True anomaly
348.14934°
Mean anomaly
349.7988°
Eccentric anomaly
348.98988°
Mean motion
3.37233 °/min
Orbital period
106.75 mins
BSTAR
0.000075212
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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 | 2026-05-22 18:53:50.462Z | 213.125° SW | 2026-05-22 18:56:50.462Z | 158.116° S | 26.748° | 2026-05-22 19:00:50.462Z | 103.456° ESE |
| 9 mins | 2026-05-22 20:45:50.462Z | 243.385° WSW | 2026-05-22 20:48:50.462Z | 187.895° SSW | 36.888° | 2026-05-22 20:54:50.462Z | 106.907° ESE |
| 11 mins | 2026-05-22 22:37:50.462Z | 253.069° W | 2026-05-22 22:41:50.462Z | 196.387° SSW | 32.838° | 2026-05-22 22:48:50.462Z | 128.811° SE |
| 10 mins | 2026-05-23 00:30:50.462Z | 244.833° WSW | 2026-05-23 00:34:50.462Z | 207.776° SW | 19.933° | 2026-05-23 00:40:50.462Z | 163.409° S |
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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