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 23275.80698230 .00001057 00000-0 13926-3 0 9994
2 32376 97.8886 97.7317 0001453 88.1968 271.9411 14.82162696855677
| Epoch (UTC): | 02 October 2023 19:22:03 |
| Eccentricity: | 0.0001453 |
| inclination: | 97.8886° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 97.7317° |
| argument of perigee: | 88.1968° |
| revolutions per day: | 14.82162696 |
| mean anomaly at epoch: | 271.9411° |
| orbit number at epoch: | 85567 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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