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 25346.88451867 .00000225 00000-0 00000-0 0 9997
2 14129 26.0564 251.1585 6064986 63.6701 345.2960 2.05870730291655
| Epoch (UTC): | 12 December 2025 21:13:42 |
| Eccentricity: | 0.6064986 |
| inclination: | 26.0564° |
| perigee height: | 3893 km |
| apogee height: | 35554 km |
| right ascension of ascending node: | 251.1585° |
| argument of perigee: | 63.6701° |
| revolutions per day: | 2.05870730 |
| mean anomaly at epoch: | 345.2960° |
| orbit number at epoch: | 29165 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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