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 64782U 26145.00522281 +.00000000 +00000-0 +82957-3 0 00002
2 64782 53.1597 247.7230 0001061 101.9143 258.1979 15.34408653 01
| Epoch (UTC): | 25 May 2026 00:07:31 |
| Eccentricity: | 0.0001061 |
| inclination: | 53.1597° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 247.7230° |
| argument of perigee: | 101.9143° |
| revolutions per day: | 15.34408653 |
| mean anomaly at epoch: | 258.1979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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