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 24281.51820109 .00057335 00000-0 16421-2 0 9994
2 42759 43.0160 308.9740 0011856 26.1643 333.9809 15.35053032404625
| Epoch (UTC): | 07 October 2024 12:26:12 |
| Eccentricity: | 0.0011856 |
| inclination: | 43.0160° |
| perigee height: | 452 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 308.9740° |
| argument of perigee: | 26.1643° |
| revolutions per day: | 15.35053032 |
| mean anomaly at epoch: | 333.9809° |
| orbit number at epoch: | 40462 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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