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 23151.41600555 .00000495 00000-0 59328-4 0 9995
2 20466 82.5010 137.7620 0021409 39.3831 320.8934 14.81897368778337
| Epoch (UTC): | 31 May 2023 09:59:02 |
| Eccentricity: | 0.0021409 |
| inclination: | 82.5010° |
| perigee height: | 608 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 137.7620° |
| argument of perigee: | 39.3831° |
| revolutions per day: | 14.81897368 |
| mean anomaly at epoch: | 320.8934° |
| orbit number at epoch: | 77833 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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