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 19325U 26065.60552867 +.00000000 +00000-0 +10374-3 0 00009
2 19325 82.9547 175.7630 0032490 312.0952 58.6152 13.77908567 06
| Epoch (UTC): | 06 March 2026 14:31:57 |
| Eccentricity: | 0.0032490 |
| inclination: | 82.9547° |
| perigee height: | 947 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 175.7630° |
| argument of perigee: | 312.0952° |
| revolutions per day: | 13.77908567 |
| mean anomaly at epoch: | 58.6152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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