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 data is extracted from the following two-line orbital elements,
1 59281U 24052B 24358.06530998 .00000401 00000-0 22591-3 0 9997
2 59281 50.0098 155.0015 0004453 97.0334 263.1088 14.27768121 39298
| Epoch (UTC): | 23 December 2024 01:34:02 |
| Eccentricity: | 0.0004453 |
| inclination: | 50.0098° |
| perigee height: | 796 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 155.0015° |
| argument of perigee: | 97.0334° |
| revolutions per day: | 14.27768121 |
| mean anomaly at epoch: | 263.1088° |
| orbit number at epoch: | 3929 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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