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 59032U 26144.86228365 +.00000000 +00000-0 +53258-4 0 00006
2 59032 43.0040 305.9940 0001106 267.9081 92.1644 15.27569119 05
| Epoch (UTC): | 24 May 2026 20:41:41 |
| Eccentricity: | 0.0001106 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 305.9940° |
| argument of perigee: | 267.9081° |
| revolutions per day: | 15.27569119 |
| mean anomaly at epoch: | 92.1644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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