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 42956U 17061B 24358.10989156 .00000286 00000-0 94966-4 0 9996
2 42956 86.3968 251.2604 0001786 83.9457 276.1942 14.34218460377243
| Epoch (UTC): | 23 December 2024 02:38:14 |
| Eccentricity: | 0.0001786 |
| inclination: | 86.3968° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 251.2604° |
| argument of perigee: | 83.9457° |
| revolutions per day: | 14.34218460 |
| mean anomaly at epoch: | 276.1942° |
| orbit number at epoch: | 37724 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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