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 23033.50558345 .00030675 00000-0 13437-2 0 9997
2 32789 97.3203 57.2626 0006677 228.3863 131.6802 15.21939353806805
Epoch (UTC): | 02 February 2023 12:08:02 |
Eccentricity: | 0.0006677 |
inclination: | 97.3203° |
perigee height: | 495 km |
apogee height: | 504 km |
right ascension of ascending node: | 57.2626° |
argument of perigee: | 228.3863° |
revolutions per day: | 15.21939353 |
mean anomaly at epoch: | 131.6802° |
orbit number at epoch: | 80680 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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