TIMATION 1, 2847
Orbit data source: Space-Track
TIMATION 1, 2847 is a payload satellite owned by NRL (US) in LEO that was launched on Wed, 31 May 1967 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.
Embed this page
2847 intel report (Beta)
Create New Watchlist
Edit Public Description
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 TIMATION 1
1 2847U 67053E 25325.30893404 .00000268 00000-0 20804-3 0 9993
2 2847 69.9647 297.5121 0008557 314.8081 45.2331 14.02876180984636TLE epoch observation values (Epoch: 2025-11-21T07:24:51.901Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #53 in the year 1967 (1967-05-31 UTC)
TIMATION 1 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-22 07:55:00.626Z | 5.869° NNE | 2025-11-22 07:59:00.626Z | 53.098° ENE | 20.374° | 2025-11-22 08:03:00.626Z | 98.396° ESE |
| 10 mins | 2025-11-22 09:40:00.626Z | 325.827° NNW | 2025-11-22 09:44:00.626Z | 271.255° WNW | 41.03° | 2025-11-22 09:50:00.626Z | 170.853° S |
| 9 mins | 2025-11-22 22:54:00.626Z | 168.424° S | 2025-11-22 22:58:00.626Z | 101.67° ESE | 33.934° | 2025-11-22 23:03:00.626Z | 39.124° NE |
| 9 mins | 2025-11-23 00:39:00.626Z | 251.704° W | 2025-11-23 00:43:00.626Z | 304.794° NW | 26.219° | 2025-11-23 00:48:00.626Z | 4.691° 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 ascending 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 ascending order |
|---|