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.
Embed this page
2173 intel report (Beta)
Create New Watchlist
Edit Public Description
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 NIMBUS 2
1 02173U 66040A 25242.12440009 -.00000042 00000-0 11595-4 0 9996
2 02173 100.5642 87.3930 0054697 258.5929 220.2038 13.33700937884827
TLE epoch observation values (Epoch: 2025-08-30T02:59:08.167Z)
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
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. |
---|---|---|---|---|---|---|---|
12 mins | 2025-08-31 02:24:04.969Z | 23.553° NE | 2025-08-31 02:30:04.969Z | 104.114° ESE | 42.113° | 2025-08-31 02:36:04.969Z | 183.482° SSW |
8 mins | 2025-08-31 04:12:04.969Z | 341.184° N | 2025-08-31 04:16:04.969Z | 297.257° NW | 22.596° | 2025-08-31 04:20:04.969Z | 256.576° W |
11 mins | 2025-08-31 12:44:04.969Z | 125.987° SE | 2025-08-31 12:49:04.969Z | 65.295° ENE | 33.349° | 2025-08-31 12:55:04.969Z | 359.611° N |
11 mins | 2025-08-31 14:30:04.969Z | 200.57° SSW | 2025-08-31 14:35:04.969Z | 256.495° W | 31.141° | 2025-08-31 14:41:04.969Z | 324.816° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
---|
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
---|
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
---|