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 64718U 26145.32125892 +.00000000 +00000-0 +20107-3 0 00002
2 64718 70.0002 121.0713 0003597 267.9826 92.0921 14.98336275 07
| Epoch (UTC): | 25 May 2026 07:42:36 |
| Eccentricity: | 0.0003597 |
| inclination: | 70.0002° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.0713° |
| argument of perigee: | 267.9826° |
| revolutions per day: | 14.98336275 |
| mean anomaly at epoch: | 92.0921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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