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 22147.97068193 .00002798 00000-0 17175-3 0 9998
2 28647 56.9967 232.7746 0120369 347.0278 12.7670 15.07630957166889
| Epoch (UTC): | 27 May 2022 23:17:46 |
| Eccentricity: | 0.0120369 |
| inclination: | 56.9967° |
| perigee height: | 460 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 232.7746° |
| argument of perigee: | 347.0278° |
| revolutions per day: | 15.07630957 |
| mean anomaly at epoch: | 12.7670° |
| orbit number at epoch: | 16688 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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