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 25343.08638046 .00000914 00000-0 19061-3 0 9999
2 46 66.6895 26.3583 0188509 75.6803 286.5155 14.54461867429350
| Epoch (UTC): | 09 December 2025 02:04:23 |
| Eccentricity: | 0.0188509 |
| inclination: | 66.6895° |
| perigee height: | 577 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 26.3583° |
| argument of perigee: | 75.6803° |
| revolutions per day: | 14.54461867 |
| mean anomaly at epoch: | 286.5155° |
| orbit number at epoch: | 42935 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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