DMSP 5D-2 F13 (USA 109), 23533
Orbit data source: Space-Track
DMSP 5D-2 F13 (USA 109), 23533 is a payload satellite owned by USAF SMC (US) in SSO that was launched on Fri, 24 Mar 1995 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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23533 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 DMSP 5D-2 F13 (USA 109)
1 23533U 95015A 26047.51525988 .00000114 00000-0 78534-4 0 9995
2 23533 98.8095 62.6106 0007579 133.2789 20.3490 14.16993893596101TLE epoch observation values (Epoch: 2026-02-16T12:21:58.453Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #15 in the year 1995 (1995-03-24 UTC)
DMSP 5D-2 F13 (USA 109) 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-16 23:39:27.277Z | 109.353° ESE | 2026-02-16 23:43:27.277Z | 59.07° ENE | 20.039° | 2026-02-16 23:46:27.277Z | 21.355° NNE |
| 8 mins | 2026-02-17 01:19:27.277Z | 190.794° SSW | 2026-02-17 01:23:27.277Z | 271.046° WNW | 37.372° | 2026-02-17 01:27:27.277Z | 331.961° NNW |
| 9 mins | 2026-02-17 13:39:27.277Z | 20.606° NNE | 2026-02-17 13:43:27.277Z | 114.118° SE | 43.509° | 2026-02-17 13:48:27.277Z | 187.044° SSW |
| 4 mins | 2026-02-17 15:21:27.277Z | 319.733° NNW | 2026-02-17 15:23:27.277Z | 294.609° NW | 14.85° | 2026-02-17 15:25:27.277Z | 271.042° WNW |
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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