DASH 1, 589
Orbit data source: Space-Track
DASH 1, 589 is a payload satellite owned by USAF SSD (US) in LEO that was launched on Thu, 09 May 1963 UTC via an ATLAS AGENA B launch vehicle from the Air Force Western Test Range (AFWTR). 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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Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 DASH 1
1 589U 63014D 25308.70588954 -.00000005 00000-0 -35594-2 0 9995
2 589 87.3459 211.7823 0073360 201.1910 158.5899 8.65625164974397TLE epoch observation values (Epoch: 2025-11-04T16:56:28.856Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #14 in the year 1963 (1963-05-09 UTC)
DASH 1 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. |
|---|---|---|---|---|---|---|---|
| 36 mins | 2025-11-05 04:48:24.255Z | 1.003° NNE | 2025-11-05 05:07:24.255Z | 87.324° E | 41.74° | 2025-11-05 05:24:24.255Z | 162.353° S |
| 30 mins | 2025-11-05 07:37:24.255Z | 347.105° N | 2025-11-05 07:51:24.255Z | 292.731° NW | 31.947° | 2025-11-05 08:07:24.255Z | 230.266° WSW |
| 23 mins | 2025-11-05 15:19:24.255Z | 99.359° ESE | 2025-11-05 15:30:24.255Z | 60.085° ENE | 21.87° | 2025-11-05 15:42:24.255Z | 17.902° NNE |
| 36 mins | 2025-11-05 17:55:24.255Z | 175.282° S | 2025-11-05 18:12:24.255Z | 153.802° SSE | 44.962° | 2025-11-05 18:31:24.255Z | 2.299° NNE |
| 27 mins | 2025-11-05 20:50:24.255Z | 253.11° W | 2025-11-05 21:03:24.255Z | 300.685° NW | 22.39° | 2025-11-05 21:17:24.255Z | 349.979° N |
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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