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 24357.85581712 .00043131 00000-0 98197-3 0 9999
2 42759 43.0120 230.5870 0015409 202.4297 157.5888 15.42130338416383
| Epoch (UTC): | 22 December 2024 20:32:22 |
| Eccentricity: | 0.0015409 |
| inclination: | 43.0120° |
| perigee height: | 429 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 230.5870° |
| argument of perigee: | 202.4297° |
| revolutions per day: | 15.42130338 |
| mean anomaly at epoch: | 157.5888° |
| orbit number at epoch: | 41638 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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