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 43131U 18004W 22176.49359554 .00017976 00000-0 50422-3 0 9993
2 43131 97.3760 255.7914 0004597 325.5096 34.5849 15.36624332247814
| Epoch (UTC): | 25 June 2022 11:50:46 |
| Eccentricity: | 0.0004597 |
| inclination: | 97.3760° |
| perigee height: | 453 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 255.7914° |
| argument of perigee: | 325.5096° |
| revolutions per day: | 15.36624332 |
| mean anomaly at epoch: | 34.5849° |
| orbit number at epoch: | 24781 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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