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 42783U 17036U 23266.33971873 .00043634 00000-0 87185-3 0 9993
2 42783 97.1425 299.2535 0008991 105.7988 254.4254 15.46644087347931
| Epoch (UTC): | 23 September 2023 08:09:11 |
| Eccentricity: | 0.0008991 |
| inclination: | 97.1425° |
| perigee height: | 420 km |
| apogee height: | 432 km |
| right ascension of ascending node: | 299.2535° |
| argument of perigee: | 105.7988° |
| revolutions per day: | 15.46644087 |
| mean anomaly at epoch: | 254.4254° |
| orbit number at epoch: | 34793 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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