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 19460U 26065.54744257 +.00000000 +00000-0 +87574-4 0 00005
2 19460 84.9917 172.7289 0004929 83.9895 276.1860 14.34413265 05
| Epoch (UTC): | 06 March 2026 13:08:19 |
| Eccentricity: | 0.0004929 |
| inclination: | 84.9917° |
| perigee height: | 773 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 172.7289° |
| argument of perigee: | 83.9895° |
| revolutions per day: | 14.34413265 |
| mean anomaly at epoch: | 276.1860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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