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 28647U 05016B 23154.41912726 .00005641 00000-0 30154-3 0 9998
2 28647 56.9937 154.5395 0107830 300.3284 58.7125 15.11683777222964
| Epoch (UTC): | 03 June 2023 10:03:32 |
| Eccentricity: | 0.0107830 |
| inclination: | 56.9937° |
| perigee height: | 456 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 154.5395° |
| argument of perigee: | 300.3284° |
| revolutions per day: | 15.11683777 |
| mean anomaly at epoch: | 58.7125° |
| orbit number at epoch: | 22296 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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