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 64709U 26145.33376404 +.00000000 +00000-0 +36912-3 0 00001
2 64709 70.0002 121.0931 0004154 263.3509 96.7177 14.98338313 06
| Epoch (UTC): | 25 May 2026 08:00:37 |
| Eccentricity: | 0.0004154 |
| inclination: | 70.0002° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.0931° |
| argument of perigee: | 263.3509° |
| revolutions per day: | 14.98338313 |
| mean anomaly at epoch: | 96.7177° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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