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 12472U 81049A 23081.49878828 -.00000282 00000-0 00000+0 0 9998
2 12472 11.4753 324.3144 0000763 89.4802 231.1787 1.00233275111103
| Epoch (UTC): | 22 March 2023 11:58:15 |
| Eccentricity: | 0.0000763 |
| inclination: | 11.4753° |
| perigee height: | 35794 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 324.3144° |
| argument of perigee: | 89.4802° |
| revolutions per day: | 1.00233275 |
| mean anomaly at epoch: | 231.1787° |
| orbit number at epoch: | 11110 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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