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 43478U 26145.28981568 +.00000000 +00000-0 +79790-4 0 00000
2 43478 86.4470 98.0444 0002403 92.0059 268.1418 14.43280905 06
| Epoch (UTC): | 25 May 2026 06:57:20 |
| Eccentricity: | 0.0002403 |
| inclination: | 86.4470° |
| perigee height: | 746 km |
| apogee height: | 749 km |
| right ascension of ascending node: | 98.0444° |
| argument of perigee: | 92.0059° |
| revolutions per day: | 14.43280905 |
| mean anomaly at epoch: | 268.1418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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