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 59132U 26145.36517505 +.00000000 +00000-0 +12624-3 0 00001
2 59132 97.5603 280.8656 0009915 332.9432 27.1288 15.27293621 03
| Epoch (UTC): | 25 May 2026 08:45:51 |
| Eccentricity: | 0.0009915 |
| inclination: | 97.5603° |
| perigee height: | 477 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 280.8656° |
| argument of perigee: | 332.9432° |
| revolutions per day: | 15.27293621 |
| mean anomaly at epoch: | 27.1288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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