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 00012U 59001B 24255.52972242 .00003588 00000-0 20772-2 0 9993
2 00012 32.9123 331.3573 1654289 299.8901 44.7397 11.47083774457342
| Epoch (UTC): | 11 September 2024 12:42:48 |
| Eccentricity: | 0.1654289 |
| inclination: | 32.9123° |
| perigee height: | 553 km |
| apogee height: | 3301 km |
| right ascension of ascending node: | 331.3573° |
| argument of perigee: | 299.8901° |
| revolutions per day: | 11.47083774 |
| mean anomaly at epoch: | 44.7397° |
| orbit number at epoch: | 45734 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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