OPS 4078 (DMSP 4B F2), 3510
Orbit data source: Space-Track
OPS 4078 (DMSP 4B F2), 3510 is a payload satellite owned by SAMSO (US) in SSO that was launched on Wed, 23 Oct 1968 UTC via a THOR BURNER 2 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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3510 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 OPS 4078 (DMSP 4B F2)
1 03510U 68092A 26002.33137178 .00000337 00000-0 15174-3 0 9991
2 03510 98.5519 128.0905 0030838 94.1386 266.3321 14.28188274973575TLE epoch observation values (Epoch: 2026-01-02T07:57:10.521Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #92 in the year 1968 (1968-10-23 UTC)
OPS 4078 (DMSP 4B F2) 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 | 2026-01-02 20:19:14.443Z | 42.528° NE | 2026-01-02 20:23:14.443Z | 106.541° ESE | 25.809° | 2026-01-02 20:26:14.443Z | 149.527° SSE |
| 7 mins | 2026-01-02 21:59:14.443Z | 343.571° N | 2026-01-02 22:02:14.443Z | 294.496° NW | 27.777° | 2026-01-02 22:06:14.443Z | 234.345° WSW |
| 7 mins | 2026-01-03 07:38:14.443Z | 130.695° SE | 2026-01-03 07:41:14.443Z | 74.799° E | 33.994° | 2026-01-03 07:45:14.443Z | 5.14° NNE |
| 5 mins | 2026-01-03 09:19:14.443Z | 236.235° WSW | 2026-01-03 09:21:14.443Z | 267.189° W | 20.406° | 2026-01-03 09:24:14.443Z | 308.708° NW |
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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