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 41362U 00055JF 23341.27973238 .00005775 00000-0 20407-2 0 9999
2 41362 98.9527 133.9255 0046359 254.4326 105.1738 14.34451735409240
| Epoch (UTC): | 07 December 2023 06:42:48 |
| Eccentricity: | 0.0046359 |
| inclination: | 98.9527° |
| perigee height: | 744 km |
| apogee height: | 810 km |
| right ascension of ascending node: | 133.9255° |
| argument of perigee: | 254.4326° |
| revolutions per day: | 14.34451735 |
| mean anomaly at epoch: | 105.1738° |
| orbit number at epoch: | 40924 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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