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 41923U 17003G 25346.23635538 .00000178 00000-0 56453-4 0 9998
2 41923 86.3983 166.5721 0001784 89.2453 270.8947 14.34217037466451
| Epoch (UTC): | 12 December 2025 05:40:21 |
| Eccentricity: | 0.0001784 |
| inclination: | 86.3983° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 166.5721° |
| argument of perigee: | 89.2453° |
| revolutions per day: | 14.34217037 |
| mean anomaly at epoch: | 270.8947° |
| orbit number at epoch: | 46645 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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