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 23081.42783480 .00000345 00000-0 13470-3 0 9998
2 28057 98.5922 29.5560 0001790 73.9881 286.1499 14.35806653 17434
| Epoch (UTC): | 22 March 2023 10:16:04 |
| Eccentricity: | 0.0001790 |
| inclination: | 98.5922° |
| perigee height: | 771 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 29.5560° |
| argument of perigee: | 73.9881° |
| revolutions per day: | 14.35806653 |
| mean anomaly at epoch: | 286.1499° |
| orbit number at epoch: | 1743 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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