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 58985U 26145.43153931 +.00000000 +00000-0 +55447-4 0 00004
2 58985 53.1615 297.2896 0001478 82.0364 278.0806 15.34386130 09
| Epoch (UTC): | 25 May 2026 10:21:24 |
| Eccentricity: | 0.0001478 |
| inclination: | 53.1615° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 297.2896° |
| argument of perigee: | 82.0364° |
| revolutions per day: | 15.34386130 |
| mean anomaly at epoch: | 278.0806° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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