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 59529U 26144.74055147 +.00000000 +00000-0 +54918-4 0 00004
2 59529 43.0034 245.2831 0001603 273.6707 86.3962 15.27581684 04
| Epoch (UTC): | 24 May 2026 17:46:23 |
| Eccentricity: | 0.0001603 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 245.2831° |
| argument of perigee: | 273.6707° |
| revolutions per day: | 15.27581684 |
| mean anomaly at epoch: | 86.3962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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