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 24357.62043499 -.00000100 00000-0 -15443-3 0 9994
2 00053 47.2747 212.8636 0097321 275.8320 83.1382 12.17361424869456
| Epoch (UTC): | 22 December 2024 14:53:25 |
| Eccentricity: | 0.0097321 |
| inclination: | 47.2747° |
| perigee height: | 1526 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 212.8636° |
| argument of perigee: | 275.8320° |
| revolutions per day: | 12.17361424 |
| mean anomaly at epoch: | 83.1382° |
| orbit number at epoch: | 86945 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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