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 23025.74033957 -.00000113 00000-0 -26773-3 0 9998
2 00053 47.2731 202.2078 0099147 16.3706 344.0249 12.17288951784568
| Epoch (UTC): | 25 January 2023 17:46:05 |
| Eccentricity: | 0.0099147 |
| inclination: | 47.2731° |
| perigee height: | 1525 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 202.2078° |
| argument of perigee: | 16.3706° |
| revolutions per day: | 12.17288951 |
| mean anomaly at epoch: | 344.0249° |
| orbit number at epoch: | 78456 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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