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 24260.81405910 .00014859 00000-0 11764-2 0 9990
2 40032 98.0111 215.8284 0008763 170.0303 190.1095 15.00671279556402
| Epoch (UTC): | 16 September 2024 19:32:14 |
| Eccentricity: | 0.0008763 |
| inclination: | 98.0111° |
| perigee height: | 559 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 215.8284° |
| argument of perigee: | 170.0303° |
| revolutions per day: | 15.00671279 |
| mean anomaly at epoch: | 190.1095° |
| orbit number at epoch: | 55640 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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