OPS 9845 (DMSP 5D-2 F6), 13736
Orbit data source: Space-Track
OPS 9845 (DMSP 5D-2 F6), 13736 is a payload satellite owned by USAF SD (US) in SSO that was launched on Tue, 21 Dec 1982 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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13736 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 OPS 9845 (DMSP 5D-2 F6)
1 13736U 82118A 26098.27286365 .00000170 00000-0 81868-4 0 9997
2 13736 98.5940 286.7424 0007829 163.2037 196.9406 14.30494840255013TLE epoch observation values (Epoch: 2026-04-08T06:32:55.419Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #118 in the year 1982 (1982-12-21 UTC)
OPS 9845 (DMSP 5D-2 F6) 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-04-08 13:22:25.614Z | 207.519° SW | 2026-04-08 13:26:25.614Z | 260.701° W | 24.926° | 2026-04-08 13:30:25.614Z | 318.558° NNW |
| 8 mins | 2026-04-09 01:36:25.614Z | 6.852° NNE | 2026-04-09 01:39:25.614Z | 318.557° NNW | 43.445° | 2026-04-09 01:44:25.614Z | 202.171° SSW |
| 6 mins | 2026-04-09 11:15:25.614Z | 96.946° ESE | 2026-04-09 11:17:25.614Z | 70.491° E | 18.127° | 2026-04-09 11:21:25.614Z | 19.784° NNE |
| 8 mins | 2026-04-09 12:53:25.614Z | 189.066° SSW | 2026-04-09 12:57:25.614Z | 280.405° WNW | 37.807° | 2026-04-09 13:01:25.614Z | 334.758° 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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