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 26072.97834719 +.00000000 +00000-0 +38046-4 0 00005
2 20578 82.9460 150.0550 0013906 56.1390 116.4783 13.76637041 00
| Epoch (UTC): | 13 March 2026 23:28:49 |
| Eccentricity: | 0.0013906 |
| inclination: | 82.9460° |
| perigee height: | 966 km |
| apogee height: | 986 km |
| right ascension of ascending node: | 150.0550° |
| argument of perigee: | 56.1390° |
| revolutions per day: | 13.76637041 |
| mean anomaly at epoch: | 116.4783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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