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 23151.17873404 .00004803 00000-0 25965-3 0 9990
2 28647 56.9937 167.8327 0107693 294.1068 64.8738 15.11642694222470
| Epoch (UTC): | 31 May 2023 04:17:22 |
| Eccentricity: | 0.0107693 |
| inclination: | 56.9937° |
| perigee height: | 457 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 167.8327° |
| argument of perigee: | 294.1068° |
| revolutions per day: | 15.11642694 |
| mean anomaly at epoch: | 64.8738° |
| orbit number at epoch: | 22247 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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