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 00053U 60009E 22179.83858930 .00000008 00000-0 91772-3 0 9995
2 00053 47.2749 132.6306 0096896 111.4985 249.6167 12.17272284758877
| Epoch (UTC): | 28 June 2022 20:07:34 |
| Eccentricity: | 0.0096896 |
| inclination: | 47.2749° |
| perigee height: | 1527 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 132.6306° |
| argument of perigee: | 111.4985° |
| revolutions per day: | 12.17272284 |
| mean anomaly at epoch: | 249.6167° |
| orbit number at epoch: | 75887 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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