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 23150.45128720 .00004200 00000-0 22927-3 0 9990
2 28647 56.9937 170.8168 0107648 292.7200 66.2491 15.11634699222365
| Epoch (UTC): | 30 May 2023 10:49:51 |
| Eccentricity: | 0.0107648 |
| inclination: | 56.9937° |
| perigee height: | 457 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 170.8168° |
| argument of perigee: | 292.7200° |
| revolutions per day: | 15.11634699 |
| mean anomaly at epoch: | 66.2491° |
| orbit number at epoch: | 22236 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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