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 32376U 07059A 22140.62122783 .00000912 00000-0 12110-3 0 9992
2 32376 97.8877 324.6852 0001437 96.0010 264.1374 14.82159686781586
| Epoch (UTC): | 20 May 2022 14:54:34 |
| Eccentricity: | 0.0001437 |
| inclination: | 97.8877° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 324.6852° |
| argument of perigee: | 96.0010° |
| revolutions per day: | 14.82159686 |
| mean anomaly at epoch: | 264.1374° |
| orbit number at epoch: | 78158 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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