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 25137.65659360 -.00000040 00000-0 44335-3 0 9998
2 00053 47.2748 122.4105 0100253 345.6663 14.1289 12.17383990887248
| Epoch (UTC): | 17 May 2025 15:45:29 |
| Eccentricity: | 0.0100253 |
| inclination: | 47.2748° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 122.4105° |
| argument of perigee: | 345.6663° |
| revolutions per day: | 12.17383990 |
| mean anomaly at epoch: | 14.1289° |
| orbit number at epoch: | 88724 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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