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 64051U 26145.64877462 +.00000000 +00000-0 +17648-3 0 00000
2 64051 97.3831 217.4122 0000598 284.3388 75.7780 15.18213950 05
| Epoch (UTC): | 25 May 2026 15:34:14 |
| Eccentricity: | 0.0000598 |
| inclination: | 97.3831° |
| perigee height: | 511 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 217.4122° |
| argument of perigee: | 284.3388° |
| revolutions per day: | 15.18213950 |
| mean anomaly at epoch: | 75.7780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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