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 64708U 26145.38386819 +.00000000 +00000-0 -35627-5 0 00001
2 64708 69.9999 121.2880 0003441 269.1526 90.9239 14.98321341 01
| Epoch (UTC): | 25 May 2026 09:12:46 |
| Eccentricity: | 0.0003441 |
| inclination: | 69.9999° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 121.2880° |
| argument of perigee: | 269.1526° |
| revolutions per day: | 14.98321341 |
| mean anomaly at epoch: | 90.9239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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