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 14506U 83113A 24282.43828706 .00004820 00000-0 19137-2 0 9995
2 14506 98.3451 79.9140 0009930 250.9912 167.6213 14.29163629127376
| Epoch (UTC): | 08 October 2024 10:31:08 |
| Eccentricity: | 0.0009930 |
| inclination: | 98.3451° |
| perigee height: | 787 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 79.9140° |
| argument of perigee: | 250.9912° |
| revolutions per day: | 14.29163629 |
| mean anomaly at epoch: | 167.6213° |
| orbit number at epoch: | 12737 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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