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 64001U 26145.41077333 +.00000000 +00000-0 +62473-3 0 00005
2 64001 42.9977 285.1263 0000369 270.9707 89.1103 15.27596682 01
| Epoch (UTC): | 25 May 2026 09:51:30 |
| Eccentricity: | 0.0000369 |
| inclination: | 42.9977° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 285.1263° |
| argument of perigee: | 270.9707° |
| revolutions per day: | 15.27596682 |
| mean anomaly at epoch: | 89.1103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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