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 25196.84050149 .00001530 00000-0 13631-3 0 9996
2 22626 82.5205 132.9962 0017589 27.3510 332.8633 14.95262946744980
| Epoch (UTC): | 15 July 2025 20:10:19 |
| Eccentricity: | 0.0017589 |
| inclination: | 82.5205° |
| perigee height: | 569 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 132.9962° |
| argument of perigee: | 27.3510° |
| revolutions per day: | 14.95262946 |
| mean anomaly at epoch: | 332.8633° |
| orbit number at epoch: | 74498 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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