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 25133.71632026 .00000015 00000-0 97545-3 0 9993
2 00053 47.2746 134.5654 0100244 333.9754 25.6016 12.17383357886768
| Epoch (UTC): | 13 May 2025 17:11:30 |
| Eccentricity: | 0.0100244 |
| inclination: | 47.2746° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 134.5654° |
| argument of perigee: | 333.9754° |
| revolutions per day: | 12.17383357 |
| mean anomaly at epoch: | 25.6016° |
| orbit number at epoch: | 88676 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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