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 43931U 26145.54998692 +.00000000 +00000-0 +16517-4 0 00007
2 43931 86.3983 3.0584 0002057 78.3981 281.7446 14.34218052 01
| Epoch (UTC): | 25 May 2026 13:11:58 |
| Eccentricity: | 0.0002057 |
| inclination: | 86.3983° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 3.0584° |
| argument of perigee: | 78.3981° |
| revolutions per day: | 14.34218052 |
| mean anomaly at epoch: | 281.7446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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