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 58809U 26145.24883569 +.00000000 +00000-0 -57597-5 0 00005
2 58809 43.0032 92.9659 0001210 263.6285 96.4429 15.27579904 03
| Epoch (UTC): | 25 May 2026 05:58:19 |
| Eccentricity: | 0.0001210 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 92.9659° |
| argument of perigee: | 263.6285° |
| revolutions per day: | 15.27579904 |
| mean anomaly at epoch: | 96.4429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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