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 20046U 89042B 23160.57862636 .00000166 00000-0 14798-3 0 9995
2 20046 82.9357 115.7554 0043446 66.0747 294.4953 13.78347844709794
| Epoch (UTC): | 09 June 2023 13:53:13 |
| Eccentricity: | 0.0043446 |
| inclination: | 82.9357° |
| perigee height: | 938 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 115.7554° |
| argument of perigee: | 66.0747° |
| revolutions per day: | 13.78347844 |
| mean anomaly at epoch: | 294.4953° |
| orbit number at epoch: | 70979 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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