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 26073.61990858 +.00000000 +00000-0 +42239-4 0 00003
2 20578 82.9459 149.5788 0013887 54.4820 55.8501 13.76637106 07
| Epoch (UTC): | 14 March 2026 14:52:40 |
| Eccentricity: | 0.0013887 |
| inclination: | 82.9459° |
| perigee height: | 966 km |
| apogee height: | 986 km |
| right ascension of ascending node: | 149.5788° |
| argument of perigee: | 54.4820° |
| revolutions per day: | 13.76637106 |
| mean anomaly at epoch: | 55.8501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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