NOAA 3, 6920
Orbit data source: Space-Track
NOAA 3, 6920 is a payload satellite owned by NOAA (US) in SSO that was launched on Tue, 06 Nov 1973 UTC via a DELTA 0300 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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6920 intel report (Beta)
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TLE from 14 hours ago
0 NOAA 3
1 06920U 73086A 25200.77052039 -.00000027 00000-0 14099-3 0 9999
2 06920 102.2891 206.4793 0006631 19.8649 153.7451 12.40383934340680
TLE epoch observation values (Epoch: 2025-07-19T18:29:32.961Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #86 in the year 1973 (1973-11-06 UTC)
NOAA 3 Visibility forecast
Observer location: undefined°, undefined°
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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10 mins | 2025-07-20 11:39:57.007Z | 54.077° ENE | 2025-07-20 11:44:57.007Z | 92.257° ESE | 17.766° | 2025-07-20 11:49:57.007Z | 130.362° SE |
15 mins | 2025-07-20 13:32:57.007Z | 17.415° NNE | 2025-07-20 13:39:57.007Z | 230.86° WSW | 44.901° | 2025-07-20 13:47:57.007Z | 201.898° SSW |
10 mins | 2025-07-20 15:27:57.007Z | 345.584° N | 2025-07-20 15:31:57.007Z | 313.626° NW | 19.892° | 2025-07-20 15:37:57.007Z | 266.881° W |
13 mins | 2025-07-20 22:44:57.007Z | 110.947° ESE | 2025-07-20 22:50:57.007Z | 59.103° ENE | 28.127° | 2025-07-20 22:57:57.007Z | 0.129° NNE |
14 mins | 2025-07-21 00:37:57.007Z | 179.619° S | 2025-07-21 00:44:57.007Z | 270.333° WNW | 41.043° | 2025-07-21 00:51:57.007Z | 333.66° NNW |
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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