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 22147.77175853 .00002809 00000-0 17236-3 0 9999
2 28647 56.9967 233.5856 0120332 346.6665 13.1201 15.07629942166859
| Epoch (UTC): | 27 May 2022 18:31:19 |
| Eccentricity: | 0.0120332 |
| inclination: | 56.9967° |
| perigee height: | 460 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 233.5856° |
| argument of perigee: | 346.6665° |
| revolutions per day: | 15.07629942 |
| mean anomaly at epoch: | 13.1201° |
| orbit number at epoch: | 16685 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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