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 32788U 08021F 23340.49779163 .00013767 00000-0 87566-3 0 9996
2 32788 97.5787 316.7960 0008743 113.8962 246.3184 15.08891428849046
| Epoch (UTC): | 06 December 2023 11:56:49 |
| Eccentricity: | 0.0008743 |
| inclination: | 97.5787° |
| perigee height: | 533 km |
| apogee height: | 545 km |
| right ascension of ascending node: | 316.7960° |
| argument of perigee: | 113.8962° |
| revolutions per day: | 15.08891428 |
| mean anomaly at epoch: | 246.3184° |
| orbit number at epoch: | 84904 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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