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 26021.40060434 +.00000000 +00000-0 -44812-4 0 00001
2 17590 71.0032 16.1425 0006167 216.4375 143.6330 14.17159505 02
| Epoch (UTC): | 21 January 2026 09:36:52 |
| Eccentricity: | 0.0006167 |
| inclination: | 71.0032° |
| perigee height: | 831 km |
| apogee height: | 839 km |
| right ascension of ascending node: | 16.1425° |
| argument of perigee: | 216.4375° |
| revolutions per day: | 14.17159505 |
| mean anomaly at epoch: | 143.6330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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