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 58925U 26145.59781730 +.00000000 +00000-0 +68536-3 0 00001
2 58925 97.3126 235.7525 0004881 170.9783 189.1569 15.71670902 01
| Epoch (UTC): | 25 May 2026 14:20:51 |
| Eccentricity: | 0.0004881 |
| inclination: | 97.3126° |
| perigee height: | 351 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 235.7525° |
| argument of perigee: | 170.9783° |
| revolutions per day: | 15.71670902 |
| mean anomaly at epoch: | 189.1569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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