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 63657U 26145.42258844 +.00000000 +00000-0 +62177-3 0 00001
2 63657 42.9969 291.7313 0001433 289.5647 70.5049 15.27590396 08
| Epoch (UTC): | 25 May 2026 10:08:31 |
| Eccentricity: | 0.0001433 |
| inclination: | 42.9969° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 291.7313° |
| argument of perigee: | 289.5647° |
| revolutions per day: | 15.27590396 |
| mean anomaly at epoch: | 70.5049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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