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 42432U 26144.97405737 +.00000000 +00000-0 +00000-0 0 00007
2 42432 0.0268 39.9707 0002787 31.0336 95.3337 1.00271889 04
| Epoch (UTC): | 24 May 2026 23:22:38 |
| Eccentricity: | 0.0002787 |
| inclination: | 0.0268° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 39.9707° |
| argument of perigee: | 31.0336° |
| revolutions per day: | 1.00271889 |
| mean anomaly at epoch: | 95.3337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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