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 60636U 24140AM 24357.94419901 .00001562 00000-0 74640-3 0 9998
2 60636 89.0086 335.7267 0052097 137.3782 223.1468 14.17983309 19372
| Epoch (UTC): | 22 December 2024 22:39:38 |
| Eccentricity: | 0.0052097 |
| inclination: | 89.0086° |
| perigee height: | 794 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 335.7267° |
| argument of perigee: | 137.3782° |
| revolutions per day: | 14.17983309 |
| mean anomaly at epoch: | 223.1468° |
| orbit number at epoch: | 1937 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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