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 07575U 26158.84049935 +.00000000 +00000-0 -23039-4 0 00003
2 07575 81.2463 357.6936 0049684 337.2567 22.6403 14.11578757 06
| Epoch (UTC): | 07 June 2026 20:10:19 |
| Eccentricity: | 0.0049684 |
| inclination: | 81.2463° |
| perigee height: | 818 km |
| apogee height: | 890 km |
| right ascension of ascending node: | 357.6936° |
| argument of perigee: | 337.2567° |
| revolutions per day: | 14.11578757 |
| mean anomaly at epoch: | 22.6403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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