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 64255U 26145.64146983 +.00000000 +00000-0 +38141-3 0 00004
2 64255 43.0014 232.8527 0001721 268.9626 91.1028 15.27589033 09
| Epoch (UTC): | 25 May 2026 15:23:42 |
| Eccentricity: | 0.0001721 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 232.8527° |
| argument of perigee: | 268.9626° |
| revolutions per day: | 15.27589033 |
| mean anomaly at epoch: | 91.1028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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