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 26140.19419279 +.00000000 +00000-0 +11544-4 0 00009
2 17590 70.9993 125.8166 0005083 346.8468 13.2522 14.17170760 04
| Epoch (UTC): | 20 May 2026 04:39:38 |
| Eccentricity: | 0.0005083 |
| inclination: | 70.9993° |
| perigee height: | 831 km |
| apogee height: | 839 km |
| right ascension of ascending node: | 125.8166° |
| argument of perigee: | 346.8468° |
| revolutions per day: | 14.17170760 |
| mean anomaly at epoch: | 13.2522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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