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 26127U 99057P 24357.86252874 .00016964 00000-0 25434-2 0 9997
2 26127 98.3905 131.8760 0078499 36.6994 113.1401 14.72577442304443
| Epoch (UTC): | 22 December 2024 20:42:02 |
| Eccentricity: | 0.0078499 |
| inclination: | 98.3905° |
| perigee height: | 597 km |
| apogee height: | 708 km |
| right ascension of ascending node: | 131.8760° |
| argument of perigee: | 36.6994° |
| revolutions per day: | 14.72577442 |
| mean anomaly at epoch: | 113.1401° |
| orbit number at epoch: | 30444 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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