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 40057U 14034E 23332.80537471 .00006469 00000-0 79164-3 0 9991
2 40057 98.3578 173.4028 0010731 73.3132 286.9257 14.83537523507826
| Epoch (UTC): | 28 November 2023 19:19:44 |
| Eccentricity: | 0.0010731 |
| inclination: | 98.3578° |
| perigee height: | 610 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 173.4028° |
| argument of perigee: | 73.3132° |
| revolutions per day: | 14.83537523 |
| mean anomaly at epoch: | 286.9257° |
| orbit number at epoch: | 50782 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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