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 41334U 16010A 24272.84661908 0.00000000 00000-0 00000-0 0 05
2 41334 122.9818 62.2745 0006584 350.0160 9.9840 13.41445155 05
| Epoch (UTC): | 28 September 2024 20:19:07 |
| Eccentricity: | 0.0006584 |
| inclination: | 122.9818° |
| perigee height: | 1099 km |
| apogee height: | 1109 km |
| right ascension of ascending node: | 62.2745° |
| argument of perigee: | 350.0160° |
| revolutions per day: | 13.41445155 |
| mean anomaly at epoch: | 9.9840° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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