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 43924U 26145.31531192 +.00000000 +00000-0 +14791-4 0 00004
2 43924 86.3987 3.2366 0002165 87.2388 272.9056 14.34217871 04
| Epoch (UTC): | 25 May 2026 07:34:02 |
| Eccentricity: | 0.0002165 |
| inclination: | 86.3987° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 3.2366° |
| argument of perigee: | 87.2388° |
| revolutions per day: | 14.34217871 |
| mean anomaly at epoch: | 272.9056° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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