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 23084.83751814 .00019210 00000-0 99725-3 0 9994
2 42759 43.0163 218.4960 0011938 282.4514 209.4825 15.15737357318987
| Epoch (UTC): | 25 March 2023 20:06:01 |
| Eccentricity: | 0.0011938 |
| inclination: | 43.0163° |
| perigee height: | 510 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 218.4960° |
| argument of perigee: | 282.4514° |
| revolutions per day: | 15.15737357 |
| mean anomaly at epoch: | 209.4825° |
| orbit number at epoch: | 31898 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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