OV2-3, 13912
Orbit data source: Space-Track
OV2-3, 13912 is a payload satellite owned by USAF SSD (US) in HEO that was launched on Tue, 21 Dec 1965 UTC via a TITAN IIIC launch vehicle from the Air Force Eastern Test Range (AFETR). 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
13912 intel report (Beta)
Create New Watchlist
Edit Public Description
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OV2-3
1 13912U 65108V 26032.47781727 .00016151 00000-0 10803-2 0 9990
2 13912 26.5876 215.3126 5249422 288.3983 22.9775 5.27151136563514TLE epoch observation values (Epoch: 2026-02-01T11:28:03.412Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #108 in the year 1965 (1965-12-21 UTC)
OV2-3 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. |
|---|---|---|---|---|---|---|---|
| 112 mins | 2026-02-03 19:49:01.358Z | 203.546° SW | 2026-02-03 19:55:01.358Z | 197.479° SSW | 42.902° | 2026-02-03 21:41:01.358Z | 130.572° SE |
| 112 mins | 2026-02-04 00:26:01.358Z | 280.909° WNW | 2026-02-04 01:40:01.358Z | 255.923° W | 17.32° | 2026-02-04 02:18:01.358Z | 219.758° SW |
| 80 mins | 2026-02-04 12:22:01.358Z | 160.639° S | 2026-02-04 12:37:01.358Z | 116.876° SE | 23.496° | 2026-02-04 13:42:01.358Z | 78.014° E |
| 164 mins | 2026-02-04 17:05:01.358Z | 247.449° WSW | 2026-02-04 18:03:01.358Z | 175.396° S | 43.267° | 2026-02-04 19:49:01.358Z | 121.663° SE |
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 |
|---|