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 20322U 26150.49822838 +.00000000 +00000-0 -53480-4 0 00005
2 20322 98.8955 152.9136 0009434 125.5494 37.3591 14.05460250 07
| Epoch (UTC): | 30 May 2026 11:57:26 |
| Eccentricity: | 0.0009434 |
| inclination: | 98.8955° |
| perigee height: | 868 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 152.9136° |
| argument of perigee: | 125.5494° |
| revolutions per day: | 14.05460250 |
| mean anomaly at epoch: | 37.3591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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