QPS-SAR-11 YAMATSUMI, 64340
Orbit data source: Space-Track
QPS-SAR-11 YAMATSUMI, 64340 is a payload satellite owned by QPS Labs (JP) in LEO that was launched on Wed, 11 Jun 2025 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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64340 intel report (Beta)
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TLE from 11 hours ago
0 QPS-SAR-11 YAMATSUMI
1 64340U 25125A 25211.56775329 .00006116 00000-0 53175-3 0 9995
2 64340 42.0084 159.6654 0008715 234.2955 125.7059 14.97421376 7330
TLE epoch observation values (Epoch: 2025-07-30T13:37:33.884Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #125 in the year 2025 (2025-06-11 UTC)
QPS-SAR-11 YAMATSUMI Visibility forecast
Observer location: undefined°, undefined°
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. |
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7 mins | 2025-07-31 01:05:15.852Z | 247.569° W | 2025-07-31 01:08:15.852Z | 222.365° SW | 43.285° | 2025-07-31 01:12:15.852Z | 76.254° E |
6 mins | 2025-07-31 02:47:15.852Z | 282.082° WNW | 2025-07-31 02:50:15.852Z | 28.968° NE | 41.528° | 2025-07-31 02:53:15.852Z | 80.192° E |
7 mins | 2025-07-31 04:28:15.852Z | 283.317° WNW | 2025-07-31 04:31:15.852Z | 174.086° S | 44.633° | 2025-07-31 04:35:15.852Z | 110.965° ESE |
5 mins | 2025-07-31 06:10:15.852Z | 247.755° W | 2025-07-31 06:12:15.852Z | 206.157° SW | 22.542° | 2025-07-31 06:15:15.852Z | 160.026° S |
6 mins | 2025-07-31 23:27:15.852Z | 205.702° SW | 2025-07-31 23:30:15.852Z | 137.788° SSE | 29.195° | 2025-07-31 23:33:15.852Z | 88.082° E |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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