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 42956U 26145.42021632 +.00000000 +00000-0 +44758-5 0 00000
2 42956 86.3988 34.7034 0002189 84.2470 275.8976 14.34217827 09
| Epoch (UTC): | 25 May 2026 10:05:06 |
| Eccentricity: | 0.0002189 |
| inclination: | 86.3988° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 34.7034° |
| argument of perigee: | 84.2470° |
| revolutions per day: | 14.34217827 |
| mean anomaly at epoch: | 275.8976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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