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 23086.09635225 .00014343 00000-0 74752-3 0 9996
2 42759 43.0162 211.5143 0011960 290.4563 238.5218 15.15766256319172
| Epoch (UTC): | 27 March 2023 02:18:44 |
| Eccentricity: | 0.0011960 |
| inclination: | 43.0162° |
| perigee height: | 510 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 211.5143° |
| argument of perigee: | 290.4563° |
| revolutions per day: | 15.15766256 |
| mean anomaly at epoch: | 238.5218° |
| orbit number at epoch: | 31917 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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