TEMPSAT 1, 1512
Orbit data source: Space-Track
TEMPSAT 1, 1512 is a payload satellite owned by NRL (US) in LEO that was launched on Fri, 13 Aug 1965 UTC via a THOR ABLESTAR 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
1512 intel report (Beta)
Create New Watchlist
Edit Public Description
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 TEMPSAT 1
1 01512U 65065E 25242.92031378 .00000062 00000-0 10728-3 0 9998
2 01512 89.9804 212.7812 0069202 345.4591 68.1878 13.33570372921365
TLE epoch observation values (Epoch: 2025-08-30T22:05:15.11Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #65 in the year 1965 (1965-08-13 UTC)
TEMPSAT 1 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. |
---|---|---|---|---|---|---|---|
11 mins | 2025-08-31 09:13:29.831Z | 26.221° NE | 2025-08-31 09:19:29.831Z | 85.996° E | 24.894° | 2025-08-31 09:24:29.831Z | 134.635° SE |
12 mins | 2025-08-31 11:01:29.831Z | 348.965° N | 2025-08-31 11:07:29.831Z | 270.285° WNW | 38.03° | 2025-08-31 11:13:29.831Z | 206.964° SW |
10 mins | 2025-08-31 21:21:29.831Z | 127.999° SE | 2025-08-31 21:26:29.831Z | 69.197° E | 26.682° | 2025-08-31 21:31:29.831Z | 19.785° NNE |
11 mins | 2025-08-31 23:08:29.831Z | 208.405° SW | 2025-08-31 23:13:29.831Z | 272.312° WNW | 34.526° | 2025-08-31 23:19:29.831Z | 342.888° N |
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 |
---|