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 23341.42620383 .00010505 00000-0 66905-3 0 9990
2 32788 97.5786 317.7126 0008823 111.2937 248.9234 15.08911779849184
| Epoch (UTC): | 07 December 2023 10:13:44 |
| Eccentricity: | 0.0008823 |
| inclination: | 97.5786° |
| perigee height: | 533 km |
| apogee height: | 545 km |
| right ascension of ascending node: | 317.7126° |
| argument of perigee: | 111.2937° |
| revolutions per day: | 15.08911779 |
| mean anomaly at epoch: | 248.9234° |
| orbit number at epoch: | 84918 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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