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 64243U 26145.58335647 +.00000000 +00000-0 -26956-3 0 00003
2 64243 42.9993 106.0828 0001744 245.3157 88.2941 15.69981269 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001744 |
| inclination: | 42.9993° |
| perigee height: | 358 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 106.0828° |
| argument of perigee: | 245.3157° |
| revolutions per day: | 15.69981269 |
| mean anomaly at epoch: | 88.2941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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