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 23317.65534723 .13045468 24864-5 20295-2 0 9991
2 32789 97.2561 341.7573 0008058 236.5318 123.5208 16.33971869850692
| Epoch (UTC): | 13 November 2023 15:43:42 |
| Eccentricity: | 0.0008058 |
| inclination: | 97.2561° |
| perigee height: | 176 km |
| apogee height: | 187 km |
| right ascension of ascending node: | 341.7573° |
| argument of perigee: | 236.5318° |
| revolutions per day: | 16.33971869 |
| mean anomaly at epoch: | 123.5208° |
| orbit number at epoch: | 85069 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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