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 63643U 26145.41231044 +.00000000 +00000-0 +79995-3 0 00004
2 63643 42.9902 291.6535 0001779 135.4762 224.6232 15.27613336 01
| Epoch (UTC): | 25 May 2026 09:53:43 |
| Eccentricity: | 0.0001779 |
| inclination: | 42.9902° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 291.6535° |
| argument of perigee: | 135.4762° |
| revolutions per day: | 15.27613336 |
| mean anomaly at epoch: | 224.6232° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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