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 28366U 04025A 23273.51773924 .00000295 00000-0 10641-3 0 9992
2 28366 98.1037 122.0500 0107236 0.6915 359.4402 14.37077084 9327
| Epoch (UTC): | 30 September 2023 12:25:32 |
| Eccentricity: | 0.0107236 |
| inclination: | 98.1037° |
| perigee height: | 691 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 122.0500° |
| argument of perigee: | 0.6915° |
| revolutions per day: | 14.37077084 |
| mean anomaly at epoch: | 359.4402° |
| orbit number at epoch: | 932 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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