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 43075U 26145.24211852 +.00000000 +00000-0 -81275-4 0 00003
2 43075 86.3955 331.6637 0002075 85.3598 274.7835 14.34215626 08
| Epoch (UTC): | 25 May 2026 05:48:39 |
| Eccentricity: | 0.0002075 |
| inclination: | 86.3955° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 331.6637° |
| argument of perigee: | 85.3598° |
| revolutions per day: | 14.34215626 |
| mean anomaly at epoch: | 274.7835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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