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 63427U 25066A 25094.61586442 .00010823 00000-0 12937-3 0 9996
2 63427 89.6759 318.3003 0074001 97.4684 319.2422 15.57450931 548
| Epoch (UTC): | 04 April 2025 14:46:50 |
| Eccentricity: | 0.0074001 |
| inclination: | 89.6759° |
| perigee height: | 345 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 318.3003° |
| argument of perigee: | 97.4684° |
| revolutions per day: | 15.57450931 |
| mean anomaly at epoch: | 319.2422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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