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 23028.77787020 -.00000058 00000-0 27430-3 0 9999
2 00053 47.2734 192.8391 0099030 25.3398 335.2203 12.17288928784938
| Epoch (UTC): | 28 January 2023 18:40:07 |
| Eccentricity: | 0.0099030 |
| inclination: | 47.2734° |
| perigee height: | 1525 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 192.8391° |
| argument of perigee: | 25.3398° |
| revolutions per day: | 12.17288928 |
| mean anomaly at epoch: | 335.2203° |
| orbit number at epoch: | 78493 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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