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 23150.78194538 .00004536 00000-0 24621-3 0 9991
2 28647 56.9937 169.4605 0107674 293.3530 65.6211 15.11638330222412
| Epoch (UTC): | 30 May 2023 18:46:00 |
| Eccentricity: | 0.0107674 |
| inclination: | 56.9937° |
| perigee height: | 457 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 169.4605° |
| argument of perigee: | 293.3530° |
| revolutions per day: | 15.11638330 |
| mean anomaly at epoch: | 65.6211° |
| orbit number at epoch: | 22241 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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