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 32443U 99025DBF 23078.59613602 .00015919 00000-0 64187-2 0 9996
2 32443 102.1175 31.5259 0079772 68.3354 292.6285 14.26353959812632
| Epoch (UTC): | 19 March 2023 14:18:26 |
| Eccentricity: | 0.0079772 |
| inclination: | 102.1175° |
| perigee height: | 746 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 31.5259° |
| argument of perigee: | 68.3354° |
| revolutions per day: | 14.26353959 |
| mean anomaly at epoch: | 292.6285° |
| orbit number at epoch: | 81263 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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