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 14781U 84021B 25108.86712902 .00002718 00000-0 29326-3 0 9990
2 14781 97.7504 76.2807 0008868 137.9902 222.1997 14.89180594214947
| Epoch (UTC): | 18 April 2025 20:48:39 |
| Eccentricity: | 0.0008868 |
| inclination: | 97.7504° |
| perigee height: | 594 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 76.2807° |
| argument of perigee: | 137.9902° |
| revolutions per day: | 14.89180594 |
| mean anomaly at epoch: | 222.1997° |
| orbit number at epoch: | 21494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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