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 20624U 90046A 23151.46960787 -.00000109 00000-0 -32258-4 0 9998
2 20624 71.0413 342.9442 0016840 305.7925 54.1632 14.14469148704611
| Epoch (UTC): | 31 May 2023 11:16:14 |
| Eccentricity: | 0.0016840 |
| inclination: | 71.0413° |
| perigee height: | 832 km |
| apogee height: | 856 km |
| right ascension of ascending node: | 342.9442° |
| argument of perigee: | 305.7925° |
| revolutions per day: | 14.14469148 |
| mean anomaly at epoch: | 54.1632° |
| orbit number at epoch: | 70461 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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