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 20433U 90004B 25194.50655640 .00000197 00000-0 73949-4 0 9990
2 20433 74.0374 340.8119 0039317 111.3031 312.1341 14.37319618858502
| Epoch (UTC): | 13 July 2025 12:09:26 |
| Eccentricity: | 0.0039317 |
| inclination: | 74.0374° |
| perigee height: | 739 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 340.8119° |
| argument of perigee: | 111.3031° |
| revolutions per day: | 14.37319618 |
| mean anomaly at epoch: | 312.1341° |
| orbit number at epoch: | 85850 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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