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 23156.58336329 .00000526 00000-0 72558-4 0 9992
2 32376 97.8882 340.2280 0001338 94.9698 265.1667 14.82168806837931
| Epoch (UTC): | 05 June 2023 14:00:02 |
| Eccentricity: | 0.0001338 |
| inclination: | 97.8882° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 340.2280° |
| argument of perigee: | 94.9698° |
| revolutions per day: | 14.82168806 |
| mean anomaly at epoch: | 265.1667° |
| orbit number at epoch: | 83793 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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