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 43137U 18004AC 22180.78750841 .00004411 00000-0 15639-3 0 9991
2 43137 97.3687 255.8338 0006291 327.6447 32.4406 15.29598010248233
| Epoch (UTC): | 29 June 2022 18:54:00 |
| Eccentricity: | 0.0006291 |
| inclination: | 97.3687° |
| perigee height: | 473 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 255.8338° |
| argument of perigee: | 327.6447° |
| revolutions per day: | 15.29598010 |
| mean anomaly at epoch: | 32.4406° |
| orbit number at epoch: | 24823 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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