SOLRAD 7A, 730
Orbit data source: Space-Track
SOLRAD 7A, 730 is an American payload satellite in LEO that was launched on Sat, 11 Jan 1964 UTC via a THOR SLV-2A AGENA D 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 SOLRAD 7A
1 00730U 64001D 26005.15683168 .00000085 00000-0 10115-3 0 9996
2 00730 69.9063 267.0132 0016601 247.0458 186.5560 13.96028777 37887TLE epoch observation values (Epoch: 2026-01-05T03:45:50.257Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #1 in the year 1964 (1964-01-11 UTC)
SOLRAD 7A 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-01-05 17:18:06.369Z | 130.558° SE | 2026-01-05 17:21:06.369Z | 98.412° ESE | 15.608° | 2026-01-05 17:24:06.369Z | 66.742° ENE |
| 10 mins | 2026-01-05 19:01:06.369Z | 212.797° SW | 2026-01-05 19:06:06.369Z | 307.849° NW | 43.572° | 2026-01-05 19:11:06.369Z | 19.633° NNE |
| 4 mins | 2026-01-05 20:51:06.369Z | 299.488° NW | 2026-01-05 20:53:06.369Z | 320.558° NNW | 12.918° | 2026-01-05 20:55:06.369Z | 340.719° N |
| 9 mins | 2026-01-06 04:04:06.369Z | 344.877° N | 2026-01-06 04:08:06.369Z | 64.543° ENE | 42.677° | 2026-01-06 04:13:06.369Z | 144.535° SSE |
| 5 mins | 2026-01-06 05:51:06.369Z | 283.288° WNW | 2026-01-06 05:53:06.369Z | 259.769° W | 16.733° | 2026-01-06 05:56:06.369Z | 226.683° WSW |
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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