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 26125U 99057M 24276.92655473 .00004910 00000-0 21550-2 0 9997
2 26125 99.2651 285.5800 0246034 223.1414 206.0764 14.09206740255048
| Epoch (UTC): | 02 October 2024 22:14:14 |
| Eccentricity: | 0.0246034 |
| inclination: | 99.2651° |
| perigee height: | 684 km |
| apogee height: | 1040 km |
| right ascension of ascending node: | 285.5800° |
| argument of perigee: | 223.1414° |
| revolutions per day: | 14.09206740 |
| mean anomaly at epoch: | 206.0764° |
| orbit number at epoch: | 25504 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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