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 17590U 87027B 25198.00738588 .00000006 00000-0 26649-4 0 9997
2 17590 71.0026 53.1169 0003438 140.1169 220.0208 14.17122639982228
| Epoch (UTC): | 17 July 2025 00:10:38 |
| Eccentricity: | 0.0003438 |
| inclination: | 71.0026° |
| perigee height: | 832 km |
| apogee height: | 837 km |
| right ascension of ascending node: | 53.1169° |
| argument of perigee: | 140.1169° |
| revolutions per day: | 14.17122639 |
| mean anomaly at epoch: | 220.0208° |
| orbit number at epoch: | 98222 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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