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 22176.12606906 .00002629 00000-0 26646-3 0 9995
2 40024 97.9856 119.7956 0012766 29.3476 330.8457 14.91757769435645
| Epoch (UTC): | 25 June 2022 03:01:32 |
| Eccentricity: | 0.0012766 |
| inclination: | 97.9856° |
| perigee height: | 583 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 119.7956° |
| argument of perigee: | 29.3476° |
| revolutions per day: | 14.91757769 |
| mean anomaly at epoch: | 330.8457° |
| orbit number at epoch: | 43564 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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