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 26241U 99057EF 24279.93922943 .00003549 00000-0 12086-2 0 9990
2 26241 98.8968 270.4226 0110666 47.6845 342.3126 14.33739203282910
| Epoch (UTC): | 05 October 2024 22:32:29 |
| Eccentricity: | 0.0110666 |
| inclination: | 98.8968° |
| perigee height: | 700 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 270.4226° |
| argument of perigee: | 47.6845° |
| revolutions per day: | 14.33739203 |
| mean anomaly at epoch: | 342.3126° |
| orbit number at epoch: | 28291 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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