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 63645U 26145.11109781 +.00000000 +00000-0 +14624-2 0 00002
2 63645 42.9998 293.6926 0001097 283.7484 76.3245 15.27590908 00
| Epoch (UTC): | 25 May 2026 02:39:58 |
| Eccentricity: | 0.0001097 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 293.6926° |
| argument of perigee: | 283.7484° |
| revolutions per day: | 15.27590908 |
| mean anomaly at epoch: | 76.3245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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