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 42759U 17034B 23085.82584450 .00015059 00000-0 78433-3 0 9994
2 42759 43.0162 213.0141 0011901 289.1946 201.9789 15.15760021319139
| Epoch (UTC): | 26 March 2023 19:49:12 |
| Eccentricity: | 0.0011901 |
| inclination: | 43.0162° |
| perigee height: | 510 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 213.0141° |
| argument of perigee: | 289.1946° |
| revolutions per day: | 15.15760021 |
| mean anomaly at epoch: | 201.9789° |
| orbit number at epoch: | 31913 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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