View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 65431U 26144.98995916 +.00000000 +00000-0 +48679-3 0 00002
2 65431 53.1591 238.1120 0000972 76.1042 284.0067 15.30208939 07
| Epoch (UTC): | 24 May 2026 23:45:32 |
| Eccentricity: | 0.0000972 |
| inclination: | 53.1591° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 238.1120° |
| argument of perigee: | 76.1042° |
| revolutions per day: | 15.30208939 |
| mean anomaly at epoch: | 284.0067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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