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 58725U 26145.22216646 +.00000000 +00000-0 +39544-4 0 00006
2 58725 53.1610 234.3864 0000908 105.1552 254.9549 15.30193281 02
| Epoch (UTC): | 25 May 2026 05:19:55 |
| Eccentricity: | 0.0000908 |
| inclination: | 53.1610° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 234.3864° |
| argument of perigee: | 105.1552° |
| revolutions per day: | 15.30193281 |
| mean anomaly at epoch: | 254.9549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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