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 41427U 00055LG 24279.51658583 .00041851 00000-0 17672-1 0 9996
2 41427 98.9293 10.2752 0035353 174.3684 185.7899 14.25021049442767
| Epoch (UTC): | 05 October 2024 12:23:53 |
| Eccentricity: | 0.0035353 |
| inclination: | 98.9293° |
| perigee height: | 783 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 10.2752° |
| argument of perigee: | 174.3684° |
| revolutions per day: | 14.25021049 |
| mean anomaly at epoch: | 185.7899° |
| orbit number at epoch: | 44276 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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