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 43924U 19002C 25322.42869595 .00000424 00000-0 14449-3 0 9991
2 43924 86.3958 81.7753 0002002 91.5501 268.5924 14.34214898358768
| Epoch (UTC): | 18 November 2025 10:17:19 |
| Eccentricity: | 0.0002002 |
| inclination: | 86.3958° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 81.7753° |
| argument of perigee: | 91.5501° |
| revolutions per day: | 14.34214898 |
| mean anomaly at epoch: | 268.5924° |
| orbit number at epoch: | 35876 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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