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 26272U 99057FJ 24357.68289696 .00011213 00000-0 17583-2 0 9998
2 26272 98.3083 63.9904 0059923 17.9480 134.6608 14.71623468308900
| Epoch (UTC): | 22 December 2024 16:23:22 |
| Eccentricity: | 0.0059923 |
| inclination: | 98.3083° |
| perigee height: | 614 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 63.9904° |
| argument of perigee: | 17.9480° |
| revolutions per day: | 14.71623468 |
| mean anomaly at epoch: | 134.6608° |
| orbit number at epoch: | 30890 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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