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 58478U 26145.31235602 +.00000000 +00000-0 +15714-3 0 00006
2 58478 43.0050 354.4223 0002125 284.1722 75.8894 15.27607542 05
| Epoch (UTC): | 25 May 2026 07:29:47 |
| Eccentricity: | 0.0002125 |
| inclination: | 43.0050° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 354.4223° |
| argument of perigee: | 284.1722° |
| revolutions per day: | 15.27607542 |
| mean anomaly at epoch: | 75.8894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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