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 58053U 26144.88396543 +.00000000 +00000-0 +73677-4 0 00001
2 58053 43.0027 316.6626 0001204 271.3461 88.7252 15.27582132 08
| Epoch (UTC): | 24 May 2026 21:12:54 |
| Eccentricity: | 0.0001204 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.6626° |
| argument of perigee: | 271.3461° |
| revolutions per day: | 15.27582132 |
| mean anomaly at epoch: | 88.7252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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