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 22626U 93024A 25198.31272743 .00001661 00000-0 14814-3 0 9995
2 22626 82.5206 131.5917 0017464 22.5351 337.6634 14.95268298745204
| Epoch (UTC): | 17 July 2025 07:30:19 |
| Eccentricity: | 0.0017464 |
| inclination: | 82.5206° |
| perigee height: | 569 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 131.5917° |
| argument of perigee: | 22.5351° |
| revolutions per day: | 14.95268298 |
| mean anomaly at epoch: | 337.6634° |
| orbit number at epoch: | 74520 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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