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 64567U 26145.58910574 +.00000000 +00000-0 +19578-3 0 00001
2 64567 97.7713 260.0020 0002363 64.7551 295.3913 14.93447522 09
| Epoch (UTC): | 25 May 2026 14:08:18 |
| Eccentricity: | 0.0002363 |
| inclination: | 97.7713° |
| perigee height: | 586 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 260.0020° |
| argument of perigee: | 64.7551° |
| revolutions per day: | 14.93447522 |
| mean anomaly at epoch: | 295.3913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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