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 27433U 02024D 24357.70954874 .00000859 00000-0 47529-3 0 9994
2 27433 98.9919 34.0082 0013741 233.6546 126.3359 14.14027902164783
| Epoch (UTC): | 22 December 2024 17:01:45 |
| Eccentricity: | 0.0013741 |
| inclination: | 98.9919° |
| perigee height: | 835 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 34.0082° |
| argument of perigee: | 233.6546° |
| revolutions per day: | 14.14027902 |
| mean anomaly at epoch: | 126.3359° |
| orbit number at epoch: | 16478 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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