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: 12 hours ago
TLE from 12 hours ago
0 DASH 1
1 00589U 63014D 26303.67849124 .00000060 00000-0 26563-1 0 9990
2 00589 87.3597 177.8103 0049210 134.2529 226.2380 8.65629195 5281TLE epoch observation values (Epoch: 2026-10-30T16:17:01.643Z)
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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-31 04:38:12.662Z | 196.014° SSW | 2026-10-31 04:38:12.662Z | 196.014° SSW | 32.525° | 2026-10-31 04:45:12.662Z | 192.426° SSW |
| 19 mins | 2026-10-31 06:59:12.662Z | 337.421° NNW | 2026-10-31 07:08:12.662Z | 305.883° NW | 18.457° | 2026-10-31 07:18:12.662Z | 270.618° WNW |
| 32 mins | 2026-10-31 14:32:12.662Z | 137.415° SSE | 2026-10-31 14:48:12.662Z | 72.235° E | 46.134° | 2026-10-31 15:04:12.662Z | 9.455° NNE |
| 35 mins | 2026-10-31 17:17:12.662Z | 207.326° SW | 2026-10-31 17:33:12.662Z | 276.241° WNW | 54.073° | 2026-10-31 17:52:12.662Z | 357.903° N |
| 34 mins | 2026-11-01 02:21:12.662Z | 5.493° NNE | 2026-11-01 02:38:12.662Z | 81.766° E | 50.005° | 2026-11-01 02:55:12.662Z | 150.75° SSE |
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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