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 00016U 58002A 23150.44547314 .00000067 00000-0 11878-3 0 9996
2 00016 34.2629 284.5520 2022653 99.1721 284.1752 10.48832584571915
| Epoch (UTC): | 30 May 2023 10:41:28 |
| Eccentricity: | 0.2022653 |
| inclination: | 34.2629° |
| perigee height: | 654 km |
| apogee height: | 4221 km |
| right ascension of ascending node: | 284.5520° |
| argument of perigee: | 99.1721° |
| revolutions per day: | 10.48832584 |
| mean anomaly at epoch: | 284.1752° |
| orbit number at epoch: | 57191 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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