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 22145.27614800 -.00000147 00000-0 -61205-3 0 9996
2 00053 47.2754 239.2222 0097006 9.7585 350.5061 12.17270738754663
| Epoch (UTC): | 25 May 2022 06:37:39 |
| Eccentricity: | 0.0097006 |
| inclination: | 47.2754° |
| perigee height: | 1527 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 239.2222° |
| argument of perigee: | 9.7585° |
| revolutions per day: | 12.17270738 |
| mean anomaly at epoch: | 350.5061° |
| orbit number at epoch: | 75466 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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