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 11U 59001A 24262.54883531 .00001456 00000-0 77280-3 0 9993
2 11 32.8684 331.9342 1454095 37.9084 331.5445 11.88734361801364
| Epoch (UTC): | 18 September 2024 13:10:19 |
| Eccentricity: | 0.1454095 |
| inclination: | 32.8684° |
| perigee height: | 552 km |
| apogee height: | 2911 km |
| right ascension of ascending node: | 331.9342° |
| argument of perigee: | 37.9084° |
| revolutions per day: | 11.88734361 |
| mean anomaly at epoch: | 331.5445° |
| orbit number at epoch: | 80136 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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