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 14129U 83058B 25108.40528335 .00000114 00000-0 00000+0 0 9992
2 14129 26.9007 290.8735 6052874 358.1859 0.2973 2.05869861286730
| Epoch (UTC): | 18 April 2025 09:43:36 |
| Eccentricity: | 0.6052874 |
| inclination: | 26.9007° |
| perigee height: | 3924 km |
| apogee height: | 35522 km |
| right ascension of ascending node: | 290.8735° |
| argument of perigee: | 358.1859° |
| revolutions per day: | 2.05869861 |
| mean anomaly at epoch: | 0.2973° |
| orbit number at epoch: | 28673 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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