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 64379U 26145.59544525 +.00000000 +00000-0 +21449-2 0 00001
2 64379 42.9999 341.3313 0002263 235.2807 124.7848 15.71011298 00
| Epoch (UTC): | 25 May 2026 14:17:26 |
| Eccentricity: | 0.0002263 |
| inclination: | 42.9999° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 341.3313° |
| argument of perigee: | 235.2807° |
| revolutions per day: | 15.71011298 |
| mean anomaly at epoch: | 124.7848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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