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 40042U 14033AJ 24280.96625494 .00036103 00000-0 24068-2 0 9997
2 40042 98.0825 250.2154 0015250 111.1210 249.1648 15.06878557560156
| Epoch (UTC): | 06 October 2024 23:11:24 |
| Eccentricity: | 0.0015250 |
| inclination: | 98.0825° |
| perigee height: | 535 km |
| apogee height: | 556 km |
| right ascension of ascending node: | 250.2154° |
| argument of perigee: | 111.1210° |
| revolutions per day: | 15.06878557 |
| mean anomaly at epoch: | 249.1648° |
| orbit number at epoch: | 56015 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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