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 64583U 26145.32844418 +.00000000 +00000-0 +72588-3 0 00004
2 64583 97.7659 259.2928 0006583 82.0309 278.1656 14.91501742 01
| Epoch (UTC): | 25 May 2026 07:52:57 |
| Eccentricity: | 0.0006583 |
| inclination: | 97.7659° |
| perigee height: | 589 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 259.2928° |
| argument of perigee: | 82.0309° |
| revolutions per day: | 14.91501742 |
| mean anomaly at epoch: | 278.1656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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