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 42075U 17016A 23272.34776465 -.00000110 00000-0 00000-0 0 9994
2 42075 0.0126 194.3528 0000364 16.4087 270.3063 1.00269391 23951
| Epoch (UTC): | 29 September 2023 08:20:46 |
| Eccentricity: | 0.0000364 |
| inclination: | 0.0126° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 194.3528° |
| argument of perigee: | 16.4087° |
| revolutions per day: | 1.00269391 |
| mean anomaly at epoch: | 270.3063° |
| orbit number at epoch: | 2395 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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