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 32791U 08021J 23087.41768874 .00009413 00000-0 85207-3 0 9990
2 32791 97.6501 60.4492 0011040 333.4187 26.6467 14.95564412809584
| Epoch (UTC): | 28 March 2023 10:01:28 |
| Eccentricity: | 0.0011040 |
| inclination: | 97.6501° |
| perigee height: | 573 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 60.4492° |
| argument of perigee: | 333.4187° |
| revolutions per day: | 14.95564412 |
| mean anomaly at epoch: | 26.6467° |
| orbit number at epoch: | 80958 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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