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 58631U 26145.62603662 +.00000000 +00000-0 +12563-4 0 00006
2 58631 43.0025 356.3918 0001038 271.0010 89.0723 15.27573946 05
| Epoch (UTC): | 25 May 2026 15:01:29 |
| Eccentricity: | 0.0001038 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.3918° |
| argument of perigee: | 271.0010° |
| revolutions per day: | 15.27573946 |
| mean anomaly at epoch: | 89.0723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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