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 20578U 26075.20732147 +.00000000 +00000-0 +37378-4 0 00003
2 20578 82.9456 148.4004 0013845 50.4493 2.4905 13.76637165 00
| Epoch (UTC): | 16 March 2026 04:58:32 |
| Eccentricity: | 0.0013845 |
| inclination: | 82.9456° |
| perigee height: | 966 km |
| apogee height: | 986 km |
| right ascension of ascending node: | 148.4004° |
| argument of perigee: | 50.4493° |
| revolutions per day: | 13.76637165 |
| mean anomaly at epoch: | 2.4905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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