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 64571U 26145.59228448 +.00000000 +00000-0 +17222-3 0 00003
2 64571 97.7702 260.0832 0002259 73.1206 287.0260 14.91860229 02
| Epoch (UTC): | 25 May 2026 14:12:53 |
| Eccentricity: | 0.0002259 |
| inclination: | 97.7702° |
| perigee height: | 591 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 260.0832° |
| argument of perigee: | 73.1206° |
| revolutions per day: | 14.91860229 |
| mean anomaly at epoch: | 287.0260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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