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 43257U 26145.40360392 +.00000000 +00000-0 -19249-4 0 00009
2 43257 86.3935 299.9957 0002051 90.9786 269.1645 14.34217630 08
| Epoch (UTC): | 25 May 2026 09:41:11 |
| Eccentricity: | 0.0002051 |
| inclination: | 86.3935° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 299.9957° |
| argument of perigee: | 90.9786° |
| revolutions per day: | 14.34217630 |
| mean anomaly at epoch: | 269.1645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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