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 43258U 26145.66364963 +.00000000 +00000-0 +26515-4 0 00009
2 43258 86.3943 299.9784 0002085 89.8889 270.2546 14.34218393 04
| Epoch (UTC): | 25 May 2026 15:55:39 |
| Eccentricity: | 0.0002085 |
| inclination: | 86.3943° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 299.9784° |
| argument of perigee: | 89.8889° |
| revolutions per day: | 14.34218393 |
| mean anomaly at epoch: | 270.2546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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