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 53U 60009E 23334.41140577 -.00000078 00000-0 56544-4 0 9991
2 53 47.2791 330.2215 0099775 208.7347 150.7921 12.17317714822162
| Epoch (UTC): | 30 November 2023 09:52:25 |
| Eccentricity: | 0.0099775 |
| inclination: | 47.2791° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 330.2215° |
| argument of perigee: | 208.7347° |
| revolutions per day: | 12.17317714 |
| mean anomaly at epoch: | 150.7921° |
| orbit number at epoch: | 82216 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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