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 35935U 09051E 24252.43170707 .00004283 00000-0 93869-3 0 9999
2 35935 98.4598 137.9161 0009263 82.0872 278.1377 14.58157354794429
| Epoch (UTC): | 08 September 2024 10:21:39 |
| Eccentricity: | 0.0009263 |
| inclination: | 98.4598° |
| perigee height: | 692 km |
| apogee height: | 705 km |
| right ascension of ascending node: | 137.9161° |
| argument of perigee: | 82.0872° |
| revolutions per day: | 14.58157354 |
| mean anomaly at epoch: | 278.1377° |
| orbit number at epoch: | 79442 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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