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 23149.98836448 .00004177 00000-0 22815-3 0 9998
2 28647 56.9938 172.7160 0107625 291.8351 67.1268 15.11631106222295
Epoch (UTC): | 29 May 2023 23:43:14 |
Eccentricity: | 0.0107625 |
inclination: | 56.9938° |
perigee height: | 457 km |
apogee height: | 605 km |
right ascension of ascending node: | 172.7160° |
argument of perigee: | 291.8351° |
revolutions per day: | 15.11631106 |
mean anomaly at epoch: | 67.1268° |
orbit number at epoch: | 22229 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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