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 26074.55079653 +.00000000 +00000-0 +32285-4 0 00008
2 17590 70.9992 264.1430 0003165 129.3462 230.7943 14.17166677 06
| Epoch (UTC): | 15 March 2026 13:13:08 |
| Eccentricity: | 0.0003165 |
| inclination: | 70.9992° |
| perigee height: | 833 km |
| apogee height: | 837 km |
| right ascension of ascending node: | 264.1430° |
| argument of perigee: | 129.3462° |
| revolutions per day: | 14.17166677 |
| mean anomaly at epoch: | 230.7943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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