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 23332.53558597 .00006494 00000-0 79472-3 0 9993
2 40057 98.3578 173.1204 0010737 74.1260 286.1135 14.83533945507782
| Epoch (UTC): | 28 November 2023 12:51:14 |
| Eccentricity: | 0.0010737 |
| inclination: | 98.3578° |
| perigee height: | 610 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 173.1204° |
| argument of perigee: | 74.1260° |
| revolutions per day: | 14.83533945 |
| mean anomaly at epoch: | 286.1135° |
| orbit number at epoch: | 50778 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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