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 14453U 83109B 24254.68528683 .00000474 00000-0 18620-3 0 9996
2 14453 81.1685 327.4103 0103613 338.1919 21.4863 14.25161030123739
| Epoch (UTC): | 10 September 2024 16:26:48 |
| Eccentricity: | 0.0103613 |
| inclination: | 81.1685° |
| perigee height: | 733 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 327.4103° |
| argument of perigee: | 338.1919° |
| revolutions per day: | 14.25161030 |
| mean anomaly at epoch: | 21.4863° |
| orbit number at epoch: | 12373 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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