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 28948U 06007D 22224.43306454 .00003114 00000-0 73405-3 0 9996
2 28948 4.5695 153.3596 7062951 119.6412 326.9365 2.55996995145786
| Epoch (UTC): | 12 August 2022 10:23:36 |
| Eccentricity: | 0.7062951 |
| inclination: | 4.5695° |
| perigee height: | 251 km |
| apogee height: | 32137 km |
| right ascension of ascending node: | 153.3596° |
| argument of perigee: | 119.6412° |
| revolutions per day: | 2.55996995 |
| mean anomaly at epoch: | 326.9365° |
| orbit number at epoch: | 14578 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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