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 58535U 26145.07317465 +.00000000 +00000-0 +30957-4 0 00008
2 58535 53.1609 66.9851 0001096 83.6146 276.4982 15.34388729 09
| Epoch (UTC): | 25 May 2026 01:45:22 |
| Eccentricity: | 0.0001096 |
| inclination: | 53.1609° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 66.9851° |
| argument of perigee: | 83.6146° |
| revolutions per day: | 15.34388729 |
| mean anomaly at epoch: | 276.4982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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