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 32791U 08021J 23342.48147738 .00004793 00000-0 39352-3 0 9997
2 32791 97.6820 310.5925 0009561 171.0207 189.1189 14.99630729847837
| Epoch (UTC): | 08 December 2023 11:33:19 |
| Eccentricity: | 0.0009561 |
| inclination: | 97.6820° |
| perigee height: | 561 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 310.5925° |
| argument of perigee: | 171.0207° |
| revolutions per day: | 14.99630729 |
| mean anomaly at epoch: | 189.1189° |
| orbit number at epoch: | 84783 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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