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 23332.47285991 .00019849 00000-0 12704-2 0 9994
2 32788 97.5786 308.8742 0008372 134.8598 225.3312 15.08581601847835
| Epoch (UTC): | 28 November 2023 11:20:55 |
| Eccentricity: | 0.0008372 |
| inclination: | 97.5786° |
| perigee height: | 535 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 308.8742° |
| argument of perigee: | 134.8598° |
| revolutions per day: | 15.08581601 |
| mean anomaly at epoch: | 225.3312° |
| orbit number at epoch: | 84783 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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