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 58131U 26145.43674222 +.00000000 +00000-0 +24876-4 0 00000
2 58131 43.0029 55.7364 0000896 265.8976 94.1773 15.27574865 05
| Epoch (UTC): | 25 May 2026 10:28:54 |
| Eccentricity: | 0.0000896 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 55.7364° |
| argument of perigee: | 265.8976° |
| revolutions per day: | 15.27574865 |
| mean anomaly at epoch: | 94.1773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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