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 23032.50747419 .00004676 00000-0 44856-3 0 9991
2 40024 98.0122 344.5980 0011868 20.9010 339.2692 14.93560667468147
| Epoch (UTC): | 01 February 2023 12:10:45 |
| Eccentricity: | 0.0011868 |
| inclination: | 98.0122° |
| perigee height: | 578 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 344.5980° |
| argument of perigee: | 20.9010° |
| revolutions per day: | 14.93560667 |
| mean anomaly at epoch: | 339.2692° |
| orbit number at epoch: | 46814 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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