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 64702U 26145.33392963 +.00000000 +00000-0 +27102-3 0 00003
2 64702 70.0006 121.0889 0003771 259.3221 100.7514 14.98336645 02
| Epoch (UTC): | 25 May 2026 08:00:51 |
| Eccentricity: | 0.0003771 |
| inclination: | 70.0006° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.0889° |
| argument of perigee: | 259.3221° |
| revolutions per day: | 14.98336645 |
| mean anomaly at epoch: | 100.7514° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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