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 46U 60007B 25322.45691934 .00001301 00000-0 26241-3 0 9991
2 46 66.6894 82.5530 0188396 91.8317 270.4381 14.54415722426358
| Epoch (UTC): | 18 November 2025 10:57:57 |
| Eccentricity: | 0.0188396 |
| inclination: | 66.6894° |
| perigee height: | 578 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 82.5530° |
| argument of perigee: | 91.8317° |
| revolutions per day: | 14.54415722 |
| mean anomaly at epoch: | 270.4381° |
| orbit number at epoch: | 42635 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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