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 23333.47984347 .00006580 00000-0 80491-3 0 9992
2 40057 98.3576 174.1087 0010712 71.3715 288.8659 14.83547072507929
| Epoch (UTC): | 29 November 2023 11:30:58 |
| Eccentricity: | 0.0010712 |
| inclination: | 98.3576° |
| perigee height: | 610 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 174.1087° |
| argument of perigee: | 71.3715° |
| revolutions per day: | 14.83547072 |
| mean anomaly at epoch: | 288.8659° |
| orbit number at epoch: | 50792 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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