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 04159U 69082AB 24278.80070681 .00000287 00000-0 34961-3 0 9990
2 04159 69.9619 65.9214 0115077 10.1898 350.1488 13.72732779753435
| Epoch (UTC): | 04 October 2024 19:13:01 |
| Eccentricity: | 0.0115077 |
| inclination: | 69.9619° |
| perigee height: | 905 km |
| apogee height: | 1074 km |
| right ascension of ascending node: | 65.9214° |
| argument of perigee: | 10.1898° |
| revolutions per day: | 13.72732779 |
| mean anomaly at epoch: | 350.1488° |
| orbit number at epoch: | 75343 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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