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 28485U 04047A 23331.92653161 .00011892 00000-0 60938-3 0 9997
2 28485 20.5545 183.0737 0009163 190.6479 169.3763 15.13961595 43584
| Epoch (UTC): | 27 November 2023 22:14:12 |
| Eccentricity: | 0.0009163 |
| inclination: | 20.5545° |
| perigee height: | 518 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 183.0737° |
| argument of perigee: | 190.6479° |
| revolutions per day: | 15.13961595 |
| mean anomaly at epoch: | 169.3763° |
| orbit number at epoch: | 4358 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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