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 64698U 26145.37132632 +.00000000 +00000-0 +58536-4 0 00002
2 64698 70.0001 121.2265 0004403 265.6981 94.3675 14.98333866 05
| Epoch (UTC): | 25 May 2026 08:54:42 |
| Eccentricity: | 0.0004403 |
| inclination: | 70.0001° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.2265° |
| argument of perigee: | 265.6981° |
| revolutions per day: | 14.98333866 |
| mean anomaly at epoch: | 94.3675° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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