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 25194.05453246 -.00000194 00000-0 -72532-4 0 9995
2 17590 71.0028 61.4464 0003561 149.2381 210.8952 14.17122967981667
| Epoch (UTC): | 13 July 2025 01:18:31 |
| Eccentricity: | 0.0003561 |
| inclination: | 71.0028° |
| perigee height: | 832 km |
| apogee height: | 837 km |
| right ascension of ascending node: | 61.4464° |
| argument of perigee: | 149.2381° |
| revolutions per day: | 14.17122967 |
| mean anomaly at epoch: | 210.8952° |
| orbit number at epoch: | 98166 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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