VANGUARD 1, 5
Orbit data source: Space-Track
VANGUARD 1, 5 is a payload satellite owned by NRL (US) in LEO that was launched on Mon, 17 Mar 1958 UTC via a VANGUARD launch vehicle from the Air Force Eastern Test Range (AFETR). 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: 11 hours ago
TLE from 11 hours ago
0 VANGUARD 1
1 00005U 58002B 25296.44128684 .00000007 00000-0 11179-4 0 9991
2 00005 34.2482 324.9912 1841574 151.0667 220.5891 10.85925080417542
TLE epoch observation values (Epoch: 2025-10-23T10:35:27.182Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #2 in the year 1958 (1958-03-17 UTC)
VANGUARD 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. |
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19 mins | 2025-10-24 02:01:33.572Z | 174.06° S | 2025-10-24 02:12:33.572Z | 141.743° SSE | 16.143° | 2025-10-24 02:20:33.572Z | 111.582° ESE |
25 mins | 2025-10-24 04:20:33.572Z | 213.976° SW | 2025-10-24 04:35:33.572Z | 157.249° SSE | 32.108° | 2025-10-24 04:45:33.572Z | 93.178° ESE |
19 mins | 2025-10-24 06:45:33.572Z | 245.055° WSW | 2025-10-24 06:57:33.572Z | 181.923° SSW | 40.362° | 2025-10-24 07:04:33.572Z | 98.352° ESE |
13 mins | 2025-10-24 09:10:33.572Z | 264.87° W | 2025-10-24 09:18:33.572Z | 199.858° SSW | 38.049° | 2025-10-24 09:23:33.572Z | 121.414° SE |
5 mins | 2025-10-24 11:35:33.572Z | 242.866° WSW | 2025-10-24 11:37:33.572Z | 219.479° SW | 15.916° | 2025-10-24 11:40:33.572Z | 179.176° S |
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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