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 24281.77846836 .00059934 00000-0 17136-2 0 9998
2 42759 43.0160 307.4885 0011892 28.0423 332.1070 15.35088444404666
| Epoch (UTC): | 07 October 2024 18:40:59 |
| Eccentricity: | 0.0011892 |
| inclination: | 43.0160° |
| perigee height: | 452 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 307.4885° |
| argument of perigee: | 28.0423° |
| revolutions per day: | 15.35088444 |
| mean anomaly at epoch: | 332.1070° |
| orbit number at epoch: | 40466 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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