NIMBUS 2, 2173
Orbit data source: Space-Track
NIMBUS 2, 2173 is a payload satellite owned by GSFC (US) in SSO that was launched on Sun, 15 May 1966 UTC via a THOR SLV-2A 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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2173 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 NIMBUS 2
1 02173U 66040A 25260.06070502 -.00000016 00000-0 63760-4 0 9998
2 02173 100.5614 105.8626 0054883 216.2231 298.6622 13.33702100887216
TLE epoch observation values (Epoch: 2025-09-17T01:27:24.913Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #40 in the year 1966 (1966-05-15 UTC)
NIMBUS 2 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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12 mins | 2025-09-18 02:29:39.398Z | 22.895° NE | 2025-09-18 02:35:39.398Z | 111.017° ESE | 42.525° | 2025-09-18 02:41:39.398Z | 185.246° SSW |
8 mins | 2025-09-18 04:17:39.398Z | 340.003° N | 2025-09-18 04:21:39.398Z | 295.932° NW | 21.394° | 2025-09-18 04:25:39.398Z | 256.489° W |
11 mins | 2025-09-18 12:49:39.398Z | 127.264° SE | 2025-09-18 12:54:39.398Z | 65.154° ENE | 34.2° | 2025-09-18 13:00:39.398Z | 358.975° N |
11 mins | 2025-09-18 14:35:39.398Z | 202.047° SSW | 2025-09-18 14:40:39.398Z | 256.934° W | 30.389° | 2025-09-18 14:46:39.398Z | 324.095° NNW |
10 mins | 2025-09-19 01:55:39.398Z | 41.024° NE | 2025-09-19 02:00:39.398Z | 106.685° ESE | 30.451° | 2025-09-19 02:05:39.398Z | 160.685° 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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