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 64705U 26145.36298358 +.00000000 +00000-0 +24127-3 0 00006
2 64705 70.0002 121.2201 0004052 264.5326 95.5371 14.98337276 01
| Epoch (UTC): | 25 May 2026 08:42:41 |
| Eccentricity: | 0.0004052 |
| inclination: | 70.0002° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.2201° |
| argument of perigee: | 264.5326° |
| revolutions per day: | 14.98337276 |
| mean anomaly at epoch: | 95.5371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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