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 25340.65926170 -.00000058 00000-0 25986-3 0 9990
2 00053 47.2754 216.2258 0097361 227.0258 132.2336 12.17394753911976
| Epoch (UTC): | 06 December 2025 15:49:20 |
| Eccentricity: | 0.0097361 |
| inclination: | 47.2754° |
| perigee height: | 1526 km |
| apogee height: | 1681 km |
| right ascension of ascending node: | 216.2258° |
| argument of perigee: | 227.0258° |
| revolutions per day: | 12.17394753 |
| mean anomaly at epoch: | 132.2336° |
| orbit number at epoch: | 91197 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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