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 41367U 00055JL 23341.21924582 .00004854 00000-0 18170-2 0 9997
2 41367 98.9956 134.1388 0046220 11.7895 348.4358 14.31645946406796
| Epoch (UTC): | 07 December 2023 05:15:42 |
| Eccentricity: | 0.0046220 |
| inclination: | 98.9956° |
| perigee height: | 753 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 134.1388° |
| argument of perigee: | 11.7895° |
| revolutions per day: | 14.31645946 |
| mean anomaly at epoch: | 348.4358° |
| orbit number at epoch: | 40679 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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