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 64356U 26145.36809035 +.00000000 +00000-0 +28502-3 0 00009
2 64356 70.0005 201.2773 0003841 268.9135 91.1584 14.98336956 02
| Epoch (UTC): | 25 May 2026 08:50:03 |
| Eccentricity: | 0.0003841 |
| inclination: | 70.0005° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 201.2773° |
| argument of perigee: | 268.9135° |
| revolutions per day: | 14.98336956 |
| mean anomaly at epoch: | 91.1584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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