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 64363U 26145.58086434 +.00000000 +00000-0 +19717-3 0 00009
2 64363 70.0005 200.4149 0004135 266.4828 93.5858 14.98335275 00
| Epoch (UTC): | 25 May 2026 13:56:26 |
| Eccentricity: | 0.0004135 |
| inclination: | 70.0005° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 200.4149° |
| argument of perigee: | 266.4828° |
| revolutions per day: | 14.98335275 |
| mean anomaly at epoch: | 93.5858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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