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 00011U 59001A 24255.57350130 .00001884 00000-0 99254-3 0 9992
2 00011 32.8720 358.2618 1454177 358.3136 1.2893 11.88708629458793
| Epoch (UTC): | 11 September 2024 13:45:50 |
| Eccentricity: | 0.1454177 |
| inclination: | 32.8720° |
| perigee height: | 552 km |
| apogee height: | 2911 km |
| right ascension of ascending node: | 358.2618° |
| argument of perigee: | 358.3136° |
| revolutions per day: | 11.88708629 |
| mean anomaly at epoch: | 1.2893° |
| orbit number at epoch: | 45879 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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