OPS 4467 B, 813
Orbit data source: Space-Track
OPS 4467 B, 813 is an American payload satellite in SSO that was launched on Thu, 18 Jun 1964 UTC via a THOR SLV-2 AGENA D 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.
Request partner network tasking
Embed this page
813 intel report (Beta)
Edit Public Description
Create New Watchlist
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 OPS 4467 B
1 00813U 64031B 26105.88521690 .00000018 00000-0 31328-4 0 9999
2 00813 99.8186 251.4384 0005171 0.1292 359.9884 14.23701882206066TLE epoch observation values (Epoch: 2026-04-15T21:14:42.740Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #31 in the year 1964 (1964-06-18 UTC)
OPS 4467 B Visibility forecast
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-16 10:52:34.716Z | 235.504° WSW | 2026-04-16 10:54:34.716Z | 260.766° W | 16.419° | 2026-04-16 10:57:34.716Z | 299.349° NW |
| 5 mins | 2026-04-16 21:29:34.716Z | 69.414° E | 2026-04-16 21:31:34.716Z | 98.07° ESE | 18.468° | 2026-04-16 21:34:34.716Z | 135.6° SSE |
| 8 mins | 2026-04-16 23:07:34.716Z | 359.605° N | 2026-04-16 23:11:34.716Z | 282.56° WNW | 37.708° | 2026-04-16 23:15:34.716Z | 219.047° SW |
| 8 mins | 2026-04-17 08:48:34.716Z | 123.629° SE | 2026-04-17 08:52:34.716Z | 55.263° ENE | 29.475° | 2026-04-17 08:56:34.716Z | 4.176° NNE |
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 descending order |
|---|
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 descending order |
|---|