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 22144.80686325 .00000826 00000-0 11034-3 0 9991
2 32376 97.8886 328.8102 0001421 94.3657 265.7716 14.82164794782204
| Epoch (UTC): | 24 May 2022 19:21:52 |
| Eccentricity: | 0.0001421 |
| inclination: | 97.8886° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 328.8102° |
| argument of perigee: | 94.3657° |
| revolutions per day: | 14.82164794 |
| mean anomaly at epoch: | 265.7716° |
| orbit number at epoch: | 78220 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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