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 41279U 00055GF 24261.43967563 .00021151 00000-0 11408-1 0 9996
2 41279 98.7966 320.3013 0031630 291.6897 68.0908 14.12398796448554
| Epoch (UTC): | 17 September 2024 10:33:07 |
| Eccentricity: | 0.0031630 |
| inclination: | 98.7966° |
| perigee height: | 828 km |
| apogee height: | 874 km |
| right ascension of ascending node: | 320.3013° |
| argument of perigee: | 291.6897° |
| revolutions per day: | 14.12398796 |
| mean anomaly at epoch: | 68.0908° |
| orbit number at epoch: | 44855 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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