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 59296U 26145.47696169 +.00000000 +00000-0 -12285-3 0 00002
2 59296 43.0035 153.1134 0001676 303.7345 56.3347 15.27625521 05
| Epoch (UTC): | 25 May 2026 11:26:49 |
| Eccentricity: | 0.0001676 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.1134° |
| argument of perigee: | 303.7345° |
| revolutions per day: | 15.27625521 |
| mean anomaly at epoch: | 56.3347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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