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 64573U 26145.23233679 +.00000000 +00000-0 +87903-4 0 00002
2 64573 97.7083 259.6200 0002377 31.2960 328.8404 14.99184136 00
| Epoch (UTC): | 25 May 2026 05:34:33 |
| Eccentricity: | 0.0002377 |
| inclination: | 97.7083° |
| perigee height: | 568 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 259.6200° |
| argument of perigee: | 31.2960° |
| revolutions per day: | 14.99184136 |
| mean anomaly at epoch: | 328.8404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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