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 42373U 00055RR 24355.58522135 .00063687 00000-0 75865-2 0 9992
2 42373 98.9817 275.7482 0044540 57.4989 303.0514 14.83304930467713
| Epoch (UTC): | 20 December 2024 14:02:43 |
| Eccentricity: | 0.0044540 |
| inclination: | 98.9817° |
| perigee height: | 588 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 275.7482° |
| argument of perigee: | 57.4989° |
| revolutions per day: | 14.83304930 |
| mean anomaly at epoch: | 303.0514° |
| orbit number at epoch: | 46771 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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