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 00020U 59007A 23091.85013084 .00004005 00000-0 16105-2 0 9991
2 00020 33.3539 151.9922 1659868 272.0773 69.1442 11.57208748348486
| Epoch (UTC): | 01 April 2023 20:24:11 |
| Eccentricity: | 0.1659868 |
| inclination: | 33.3539° |
| perigee height: | 508 km |
| apogee height: | 3249 km |
| right ascension of ascending node: | 151.9922° |
| argument of perigee: | 272.0773° |
| revolutions per day: | 11.57208748 |
| mean anomaly at epoch: | 69.1442° |
| orbit number at epoch: | 34848 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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