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 24286.34502370 .00018996 00000-0 14639-2 0 9994
2 40032 98.0159 242.1602 0012792 92.4862 267.7826 15.01610591560235
| Epoch (UTC): | 12 October 2024 08:16:50 |
| Eccentricity: | 0.0012792 |
| inclination: | 98.0159° |
| perigee height: | 553 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 242.1602° |
| argument of perigee: | 92.4862° |
| revolutions per day: | 15.01610591 |
| mean anomaly at epoch: | 267.7826° |
| orbit number at epoch: | 56023 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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