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.
Embed this page
1778 intel report (Beta)
Create New Watchlist
Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 A-1 (ASTERIX)
1 01778U 65096A 25259.04198379 .00000783 00000-0 21555-3 0 9992
2 01778 34.2536 121.0479 0740312 62.2773 305.0985 13.49412600927734
TLE epoch observation values (Epoch: 2025-09-16T01:00:27.399Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #96 in the year 1965 (1965-11-26 UTC)
A-1 (ASTERIX) Visibility forecast
Loading observer location...
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. |
---|---|---|---|---|---|---|---|
4 mins | 2025-09-17 18:05:47.401Z | 189.369° SSW | 2025-09-17 18:07:47.401Z | 154.809° SSE | 15.973° | 2025-09-17 18:09:47.401Z | 121.894° SE |
5 mins | 2025-09-17 19:57:47.401Z | 222.198° SW | 2025-09-17 19:59:47.401Z | 167.461° S | 29.047° | 2025-09-17 20:02:47.401Z | 110.758° ESE |
6 mins | 2025-09-17 21:49:47.401Z | 237.718° WSW | 2025-09-17 21:51:47.401Z | 190.229° SSW | 28.376° | 2025-09-17 21:55:47.401Z | 125.582° SE |
4 mins | 2025-09-17 23:42:47.401Z | 221.522° SW | 2025-09-17 23:43:47.401Z | 206.523° SW | 16.074° | 2025-09-17 23:46:47.401Z | 167.775° 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 ascending order |
---|
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
---|