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 23154.45451558 .00000527 00000-0 63455-4 0 9991
2 20466 82.5012 134.9158 0021178 29.8598 330.3819 14.81900592799842
| Epoch (UTC): | 03 June 2023 10:54:30 |
| Eccentricity: | 0.0021178 |
| inclination: | 82.5012° |
| perigee height: | 608 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 134.9158° |
| argument of perigee: | 29.8598° |
| revolutions per day: | 14.81900592 |
| mean anomaly at epoch: | 330.3819° |
| orbit number at epoch: | 79984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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