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 64310U 26145.59127163 +.00000000 +00000-0 +24102-2 0 00000
2 64310 70.0019 0.7208 0002114 275.8985 84.1933 14.98302908 04
| Epoch (UTC): | 25 May 2026 14:11:25 |
| Eccentricity: | 0.0002114 |
| inclination: | 70.0019° |
| perigee height: | 571 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 0.7208° |
| argument of perigee: | 275.8985° |
| revolutions per day: | 14.98302908 |
| mean anomaly at epoch: | 84.1933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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