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 32789U 08021G 23155.59369883 .00048323 00000-0 14030-2 0 9997
2 32789 97.3028 177.1769 0008963 151.0275 209.1468 15.35303522825458
| Epoch (UTC): | 04 June 2023 14:14:55 |
| Eccentricity: | 0.0008963 |
| inclination: | 97.3028° |
| perigee height: | 454 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 177.1769° |
| argument of perigee: | 151.0275° |
| revolutions per day: | 15.35303522 |
| mean anomaly at epoch: | 209.1468° |
| orbit number at epoch: | 82545 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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