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 00059U 60013B 24280.76109544 .00000332 00000-0 32128-3 0 9993
2 00059 28.2486 61.1129 0188859 163.8306 196.8366 13.53096213159346
| Epoch (UTC): | 06 October 2024 18:15:58 |
| Eccentricity: | 0.0188859 |
| inclination: | 28.2486° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 61.1129° |
| argument of perigee: | 163.8306° |
| revolutions per day: | 13.53096213 |
| mean anomaly at epoch: | 196.8366° |
| orbit number at epoch: | 15934 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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