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 23148.11830387 .00003816 00000-0 34792-3 0 9996
2 40024 98.0267 102.7453 0010748 358.5551 1.5636 14.95706466485936
| Epoch (UTC): | 28 May 2023 02:50:21 |
| Eccentricity: | 0.0010748 |
| inclination: | 98.0267° |
| perigee height: | 573 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 102.7453° |
| argument of perigee: | 358.5551° |
| revolutions per day: | 14.95706466 |
| mean anomaly at epoch: | 1.5636° |
| orbit number at epoch: | 48593 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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