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 26071.93917242 +.00000000 +00000-0 +47083-4 0 00004
2 17590 70.9996 269.6471 0003229 135.5963 224.5420 14.17166601 09
| Epoch (UTC): | 12 March 2026 22:32:24 |
| Eccentricity: | 0.0003229 |
| inclination: | 70.9996° |
| perigee height: | 833 km |
| apogee height: | 837 km |
| right ascension of ascending node: | 269.6471° |
| argument of perigee: | 135.5963° |
| revolutions per day: | 14.17166601 |
| mean anomaly at epoch: | 224.5420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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