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 22179.47985384 .00001367 00000-0 14137-3 0 9996
2 40024 97.9862 123.1932 0012508 18.7208 341.4468 14.91771994435628
| Epoch (UTC): | 28 June 2022 11:30:59 |
| Eccentricity: | 0.0012508 |
| inclination: | 97.9862° |
| perigee height: | 583 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 123.1932° |
| argument of perigee: | 18.7208° |
| revolutions per day: | 14.91771994 |
| mean anomaly at epoch: | 341.4468° |
| orbit number at epoch: | 43562 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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