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 19574U 26018.47457036 +.00000000 +00000-0 +49592-4 0 00005
2 19574 82.5305 89.1939 0020190 200.3928 170.2134 14.85594573 05
| Epoch (UTC): | 18 January 2026 11:23:22 |
| Eccentricity: | 0.0020190 |
| inclination: | 82.5305° |
| perigee height: | 598 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 89.1939° |
| argument of perigee: | 200.3928° |
| revolutions per day: | 14.85594573 |
| mean anomaly at epoch: | 170.2134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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