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 40024U 14033Q 22177.13220821 .00002819 00000-0 28522-3 0 9991
2 40024 97.9858 120.8148 0012701 26.2768 333.9092 14.91764143435791
| Epoch (UTC): | 26 June 2022 03:10:22 |
| Eccentricity: | 0.0012701 |
| inclination: | 97.9858° |
| perigee height: | 583 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 120.8148° |
| argument of perigee: | 26.2768° |
| revolutions per day: | 14.91764143 |
| mean anomaly at epoch: | 333.9092° |
| orbit number at epoch: | 43579 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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