DMSP 5D-2 F12 (USA 106), 23233
Orbit data source: Space-Track
DMSP 5D-2 F12 (USA 106), 23233 is a payload satellite owned by USAF SMC (US) in SSO that was launched on Mon, 29 Aug 1994 UTC via an ATLAS E 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.
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23233 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 DMSP 5D-2 F12 (USA 106)
1 23233U 94057A 26296.23641026 .00000018 00000-0 30753-4 0 9998
2 23233 98.6531 342.9812 0009854 265.4471 94.5578 14.16085914660099TLE epoch observation values (Epoch: 2026-10-23T05:40:25.846Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #57 in the year 1994 (1994-08-29 UTC)
DMSP 5D-2 F12 (USA 106) Visibility forecast
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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 | 2026-10-23 14:46:32.833Z | 59.467° ENE | 2026-10-23 14:49:32.833Z | 94.451° ESE | 15.196° | 2026-10-23 14:51:32.833Z | 117.94° SE |
| 9 mins | 2026-10-23 16:26:32.833Z | 3.823° NNE | 2026-10-23 16:30:32.833Z | 261.486° W | 64.392° | 2026-10-23 16:35:32.833Z | 205.675° SW |
| 7 mins | 2026-10-24 02:10:32.833Z | 111.865° ESE | 2026-10-24 02:13:32.833Z | 71.777° E | 25.764° | 2026-10-24 02:17:32.833Z | 16.664° NNE |
| 8 mins | 2026-10-24 03:50:32.833Z | 199.901° SSW | 2026-10-24 03:54:32.833Z | 273.825° WNW | 40.756° | 2026-10-24 03:58:32.833Z | 328.564° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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