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 32357U 99025CZA 23154.13377494 .00003728 00000-0 21519-2 0 9998
2 32357 98.9249 260.4395 0550484 76.0228 40.0673 13.52735359542265
| Epoch (UTC): | 03 June 2023 03:12:38 |
| Eccentricity: | 0.0550484 |
| inclination: | 98.9249° |
| perigee height: | 652 km |
| apogee height: | 1472 km |
| right ascension of ascending node: | 260.4395° |
| argument of perigee: | 76.0228° |
| revolutions per day: | 13.52735359 |
| mean anomaly at epoch: | 40.0673° |
| orbit number at epoch: | 54226 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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