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 58415U 26145.57315341 +.00000000 +00000-0 +18437-5 0 00001
2 58415 43.0021 338.3836 0001334 270.7161 89.3538 15.27575244 02
| Epoch (UTC): | 25 May 2026 13:45:20 |
| Eccentricity: | 0.0001334 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.3836° |
| argument of perigee: | 270.7161° |
| revolutions per day: | 15.27575244 |
| mean anomaly at epoch: | 89.3538° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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