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 64344U 26145.39744581 +.00000000 +00000-0 +16724-3 0 00006
2 64344 70.0007 200.9850 0003838 267.6510 92.4209 14.98335633 01
| Epoch (UTC): | 25 May 2026 09:32:19 |
| Eccentricity: | 0.0003838 |
| inclination: | 70.0007° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 200.9850° |
| argument of perigee: | 267.6510° |
| revolutions per day: | 14.98335633 |
| mean anomaly at epoch: | 92.4209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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