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 24340.42522238 .00045469 00000-0 10868-2 0 9996
2 42759 43.0153 331.1005 0012812 77.3848 282.8440 15.40689052413690
| Epoch (UTC): | 05 December 2024 10:12:19 |
| Eccentricity: | 0.0012812 |
| inclination: | 43.0153° |
| perigee height: | 435 km |
| apogee height: | 453 km |
| right ascension of ascending node: | 331.1005° |
| argument of perigee: | 77.3848° |
| revolutions per day: | 15.40689052 |
| mean anomaly at epoch: | 282.8440° |
| orbit number at epoch: | 41369 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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