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 42075U 26144.86841780 +.00000000 +00000-0 +00000-0 0 00000
2 42075 0.0130 272.1294 0000262 58.6201 212.3328 1.00271689 08
| Epoch (UTC): | 24 May 2026 20:50:31 |
| Eccentricity: | 0.0000262 |
| inclination: | 0.0130° |
| perigee height: | 35786 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 272.1294° |
| argument of perigee: | 58.6201° |
| revolutions per day: | 1.00271689 |
| mean anomaly at epoch: | 212.3328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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