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 44909U 19096E 25164.85372102 .00000052 00000-0 17001-3 0 9996
2 44909 82.5214 224.4388 0216276 285.6810 72.0526 12.79741180255234
| Epoch (UTC): | 13 June 2025 20:29:21 |
| Eccentricity: | 0.0216276 |
| inclination: | 82.5214° |
| perigee height: | 1175 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 224.4388° |
| argument of perigee: | 285.6810° |
| revolutions per day: | 12.79741180 |
| mean anomaly at epoch: | 72.0526° |
| orbit number at epoch: | 25523 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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