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 28057U 03049A 23272.78235406 .00000294 00000-0 11690-3 0 9994
2 28057 98.6134 220.5235 0000914 127.8411 232.2857 14.35901549 44886
| Epoch (UTC): | 29 September 2023 18:46:35 |
| Eccentricity: | 0.0000914 |
| inclination: | 98.6134° |
| perigee height: | 771 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 220.5235° |
| argument of perigee: | 127.8411° |
| revolutions per day: | 14.35901549 |
| mean anomaly at epoch: | 232.2857° |
| orbit number at epoch: | 4488 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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