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 25343.03977279 -.00000029 00000-0 53752-3 0 9991
2 53 47.2750 208.8828 0097327 233.9951 125.1785 12.17394913912260
| Epoch (UTC): | 09 December 2025 00:57:16 |
| Eccentricity: | 0.0097327 |
| inclination: | 47.2750° |
| perigee height: | 1526 km |
| apogee height: | 1681 km |
| right ascension of ascending node: | 208.8828° |
| argument of perigee: | 233.9951° |
| revolutions per day: | 12.17394913 |
| mean anomaly at epoch: | 125.1785° |
| orbit number at epoch: | 91226 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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