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 58933U 26145.19136976 +.00000000 +00000-0 +11028-4 0 00007
2 58933 53.1593 314.0972 0001479 89.5663 270.5508 15.30186523 01
| Epoch (UTC): | 25 May 2026 04:35:34 |
| Eccentricity: | 0.0001479 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 314.0972° |
| argument of perigee: | 89.5663° |
| revolutions per day: | 15.30186523 |
| mean anomaly at epoch: | 270.5508° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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