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 24286.43275345 .00005474 00000-0 11624-2 0 9999
2 35933 98.4447 172.7828 0005196 345.2955 14.8092 14.59514705799729
| Epoch (UTC): | 12 October 2024 10:23:09 |
| Eccentricity: | 0.0005196 |
| inclination: | 98.4447° |
| perigee height: | 691 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 172.7828° |
| argument of perigee: | 345.2955° |
| revolutions per day: | 14.59514705 |
| mean anomaly at epoch: | 14.8092° |
| orbit number at epoch: | 79972 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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