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 22135.81033830 .00003997 00000-0 40442-3 0 9995
2 40024 97.9844 78.9695 0012696 147.6933 212.5065 14.91510522429112
| Epoch (UTC): | 15 May 2022 19:26:53 |
| Eccentricity: | 0.0012696 |
| inclination: | 97.9844° |
| perigee height: | 584 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 78.9695° |
| argument of perigee: | 147.6933° |
| revolutions per day: | 14.91510522 |
| mean anomaly at epoch: | 212.5065° |
| orbit number at epoch: | 42911 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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