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 35933U 09051C 24280.67389405 .00005514 00000-0 11724-2 0 9998
2 35933 98.4450 166.9217 0005628 2.0774 358.0447 14.59446574798888
| Epoch (UTC): | 06 October 2024 16:10:24 |
| Eccentricity: | 0.0005628 |
| inclination: | 98.4450° |
| perigee height: | 691 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 166.9217° |
| argument of perigee: | 2.0774° |
| revolutions per day: | 14.59446574 |
| mean anomaly at epoch: | 358.0447° |
| orbit number at epoch: | 79888 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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