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 27534U 02046A 24260.94218271 .00000141 00000-0 13642-3 0 9996
2 27534 82.9308 82.4058 0035150 308.0010 162.1626 13.72866577100980
| Epoch (UTC): | 16 September 2024 22:36:44 |
| Eccentricity: | 0.0035150 |
| inclination: | 82.9308° |
| perigee height: | 963 km |
| apogee height: | 1015 km |
| right ascension of ascending node: | 82.4058° |
| argument of perigee: | 308.0010° |
| revolutions per day: | 13.72866577 |
| mean anomaly at epoch: | 162.1626° |
| orbit number at epoch: | 10098 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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