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 43140U 18004AF 22181.50048121 .00047223 00000-0 66185-3 0 9997
2 43140 97.3889 269.8504 0004032 229.6299 130.4604 15.56629057249098
| Epoch (UTC): | 30 June 2022 12:00:41 |
| Eccentricity: | 0.0004032 |
| inclination: | 97.3889° |
| perigee height: | 394 km |
| apogee height: | 400 km |
| right ascension of ascending node: | 269.8504° |
| argument of perigee: | 229.6299° |
| revolutions per day: | 15.56629057 |
| mean anomaly at epoch: | 130.4604° |
| orbit number at epoch: | 24909 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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