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 58801U 26145.24626391 +.00000000 +00000-0 +56574-4 0 00007
2 58801 43.0043 92.9512 0001304 277.8579 82.2124 15.27577737 09
| Epoch (UTC): | 25 May 2026 05:54:37 |
| Eccentricity: | 0.0001304 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 92.9512° |
| argument of perigee: | 277.8579° |
| revolutions per day: | 15.27577737 |
| mean anomaly at epoch: | 82.2124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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