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 23335.84044939 .00008651 00000-0 10547-2 0 9994
2 40057 98.3578 176.5793 0010729 64.7773 295.4551 14.83583934508270
| Epoch (UTC): | 01 December 2023 20:10:14 |
| Eccentricity: | 0.0010729 |
| inclination: | 98.3578° |
| perigee height: | 610 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 176.5793° |
| argument of perigee: | 64.7773° |
| revolutions per day: | 14.83583934 |
| mean anomaly at epoch: | 295.4551° |
| orbit number at epoch: | 50827 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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