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 61975U 26145.28419661 +.00000000 +00000-0 +67250-3 0 00009
2 61975 43.0019 107.2940 0001775 269.2128 90.8521 15.27597337 04
| Epoch (UTC): | 25 May 2026 06:49:14 |
| Eccentricity: | 0.0001775 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 107.2940° |
| argument of perigee: | 269.2128° |
| revolutions per day: | 15.27597337 |
| mean anomaly at epoch: | 90.8521° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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