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 23332.35911879 -.00000106 00000-0 -21404-3 0 9992
2 00053 47.2789 336.5509 0099802 202.6533 156.9833 12.17317703821915
| Epoch (UTC): | 28 November 2023 08:37:07 |
| Eccentricity: | 0.0099802 |
| inclination: | 47.2789° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 336.5509° |
| argument of perigee: | 202.6533° |
| revolutions per day: | 12.17317703 |
| mean anomaly at epoch: | 156.9833° |
| orbit number at epoch: | 82191 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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