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 40032U 14033Y 23081.31203358 .00007468 00000-0 73957-3 0 9998
2 40032 97.9619 20.8524 0009639 210.8666 149.1986 14.92103793475530
| Epoch (UTC): | 22 March 2023 07:29:19 |
| Eccentricity: | 0.0009639 |
| inclination: | 97.9619° |
| perigee height: | 584 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 20.8524° |
| argument of perigee: | 210.8666° |
| revolutions per day: | 14.92103793 |
| mean anomaly at epoch: | 149.1986° |
| orbit number at epoch: | 47553 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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