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 42794U 17036AF 23273.93879037 .00006727 00000-0 52072-3 0 9997
2 42794 97.4740 261.1919 0112715 306.6740 52.4164 14.96815577341778
| Epoch (UTC): | 30 September 2023 22:31:51 |
| Eccentricity: | 0.0112715 |
| inclination: | 97.4740° |
| perigee height: | 498 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 261.1919° |
| argument of perigee: | 306.6740° |
| revolutions per day: | 14.96815577 |
| mean anomaly at epoch: | 52.4164° |
| orbit number at epoch: | 34177 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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