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 58136U 26145.45830340 +.00000000 +00000-0 +20141-2 0 00001
2 58136 42.9966 55.7882 0011733 216.3326 143.6734 15.37446427 05
| Epoch (UTC): | 25 May 2026 10:59:57 |
| Eccentricity: | 0.0011733 |
| inclination: | 42.9966° |
| perigee height: | 446 km |
| apogee height: | 462 km |
| right ascension of ascending node: | 55.7882° |
| argument of perigee: | 216.3326° |
| revolutions per day: | 15.37446427 |
| mean anomaly at epoch: | 143.6734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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