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 58486U 26145.57567667 +.00000000 +00000-0 +48618-4 0 00002
2 58486 43.0017 349.5450 0001740 271.1620 88.9033 15.27585387 01
| Epoch (UTC): | 25 May 2026 13:48:58 |
| Eccentricity: | 0.0001740 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 349.5450° |
| argument of perigee: | 271.1620° |
| revolutions per day: | 15.27585387 |
| mean anomaly at epoch: | 88.9033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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