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 23334.92695629 .00019951 00000-0 12732-2 0 9994
2 32788 97.5786 311.2965 0008683 127.9592 232.2422 15.08685501848308
| Epoch (UTC): | 30 November 2023 22:14:49 |
| Eccentricity: | 0.0008683 |
| inclination: | 97.5786° |
| perigee height: | 534 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 311.2965° |
| argument of perigee: | 127.9592° |
| revolutions per day: | 15.08685501 |
| mean anomaly at epoch: | 232.2422° |
| orbit number at epoch: | 84830 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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