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 data is extracted from the following two-line orbital elements,
1 20466U 90010B 21113.17192503 .00000103 00000-0 10040-4 0 9997
2 20466 82.5007 136.9304 0021567 43.3895 316.9012 14.81419716685644
| Epoch (UTC): | 23 April 2021 04:07:34 |
| Eccentricity: | 0.0021567 |
| inclination: | 82.5007° |
| perigee height: | 610 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 136.9304° |
| argument of perigee: | 43.3895° |
| revolutions per day: | 14.81419716 |
| mean anomaly at epoch: | 316.9012° |
| orbit number at epoch: | 68564 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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