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 64375U 26144.96492645 +.00000000 +00000-0 +17185-2 0 00004
2 64375 43.0028 345.2091 0002490 279.0633 80.9953 15.70907705 08
| Epoch (UTC): | 24 May 2026 23:09:29 |
| Eccentricity: | 0.0002490 |
| inclination: | 43.0028° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 345.2091° |
| argument of perigee: | 279.0633° |
| revolutions per day: | 15.70907705 |
| mean anomaly at epoch: | 80.9953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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