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 23091.84248732 .00065214 00000-0 23463-2 0 9991
2 32789 97.3132 114.2725 0008349 55.6877 304.5152 15.28327554815691
| Epoch (UTC): | 01 April 2023 20:13:10 |
| Eccentricity: | 0.0008349 |
| inclination: | 97.3132° |
| perigee height: | 475 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 114.2725° |
| argument of perigee: | 55.6877° |
| revolutions per day: | 15.28327554 |
| mean anomaly at epoch: | 304.5152° |
| orbit number at epoch: | 81569 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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