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 22178.80909951 .00001646 00000-0 16899-3 0 9995
2 40024 97.9861 122.5137 0012567 20.9201 339.2528 14.91769656435523
| Epoch (UTC): | 27 June 2022 19:25:06 |
| Eccentricity: | 0.0012567 |
| inclination: | 97.9861° |
| perigee height: | 583 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 122.5137° |
| argument of perigee: | 20.9201° |
| revolutions per day: | 14.91769656 |
| mean anomaly at epoch: | 339.2528° |
| orbit number at epoch: | 43552 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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