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 27855U 03034B 24357.94242498 -.00000100 00000-0 -14429-3 0 9996
2 27855 0.1596 84.0105 7135742 315.3903 353.5607 2.24664705175537
| Epoch (UTC): | 22 December 2024 22:37:05 |
| Eccentricity: | 0.7135742 |
| inclination: | 0.1596° |
| perigee height: | 675 km |
| apogee height: | 35818 km |
| right ascension of ascending node: | 84.0105° |
| argument of perigee: | 315.3903° |
| revolutions per day: | 2.24664705 |
| mean anomaly at epoch: | 353.5607° |
| orbit number at epoch: | 17553 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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