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 24260.95500319 .00001053 00000-0 43153-3 0 9996
2 14506 98.3423 59.3465 0010195 320.9802 153.1733 14.29098709124301
| Epoch (UTC): | 16 September 2024 22:55:12 |
| Eccentricity: | 0.0010195 |
| inclination: | 98.3423° |
| perigee height: | 787 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 59.3465° |
| argument of perigee: | 320.9802° |
| revolutions per day: | 14.29098709 |
| mean anomaly at epoch: | 153.1733° |
| orbit number at epoch: | 12430 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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