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 23432U 94083B 22148.74164970 .00000084 00000-0 39865-4 0 9990
2 23432 74.0325 234.1140 0005490 353.3424 126.3280 14.33608611434943
| Epoch (UTC): | 28 May 2022 17:47:58 |
| Eccentricity: | 0.0005490 |
| inclination: | 74.0325° |
| perigee height: | 776 km |
| apogee height: | 783 km |
| right ascension of ascending node: | 234.1140° |
| argument of perigee: | 353.3424° |
| revolutions per day: | 14.33608611 |
| mean anomaly at epoch: | 126.3280° |
| orbit number at epoch: | 43494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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