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 is defined by the following mean orbital elements,
1 17590U 26157.06382777 +.00000000 +00000-0 +13829-3 0 00002
2 17590 71.0028 90.2679 0005938 325.7141 34.3599 14.17170775 06
| Epoch (UTC): | 06 June 2026 01:31:54 |
| Eccentricity: | 0.0005938 |
| inclination: | 71.0028° |
| perigee height: | 831 km |
| apogee height: | 839 km |
| right ascension of ascending node: | 90.2679° |
| argument of perigee: | 325.7141° |
| revolutions per day: | 14.17170775 |
| mean anomaly at epoch: | 34.3599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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