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 41364U 00055JH 23338.59306246 .00004681 00000-0 22514-2 0 9997
2 41364 98.6827 30.0282 0014586 307.8822 52.1034 14.19205315403990
| Epoch (UTC): | 04 December 2023 14:14:00 |
| Eccentricity: | 0.0014586 |
| inclination: | 98.6827° |
| perigee height: | 817 km |
| apogee height: | 838 km |
| right ascension of ascending node: | 30.0282° |
| argument of perigee: | 307.8822° |
| revolutions per day: | 14.19205315 |
| mean anomaly at epoch: | 52.1034° |
| orbit number at epoch: | 40399 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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