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 43481U 26145.36998064 +.00000000 +00000-0 +23348-4 0 00000
2 43481 86.3949 97.9678 0002499 92.6470 267.5012 14.34217957 05
| Epoch (UTC): | 25 May 2026 08:52:46 |
| Eccentricity: | 0.0002499 |
| inclination: | 86.3949° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 97.9678° |
| argument of perigee: | 92.6470° |
| revolutions per day: | 14.34217957 |
| mean anomaly at epoch: | 267.5012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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