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 58608U 26145.54196875 +.00000000 +00000-0 -60312-4 0 00000
2 58608 43.0031 94.8886 0000748 317.5847 42.4946 15.27586068 04
| Epoch (UTC): | 25 May 2026 13:00:26 |
| Eccentricity: | 0.0000748 |
| inclination: | 43.0031° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 94.8886° |
| argument of perigee: | 317.5847° |
| revolutions per day: | 15.27586068 |
| mean anomaly at epoch: | 42.4946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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