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 is defined by the following mean orbital elements,
1 47853U 98067RZ 24068.70028413 .08336335 12783-4 73058-4 0 9995
2 47853 51.6068 355.5929 0003822 13.1809 68.7005 16.51547366170884
| Epoch (UTC): | 08 March 2024 16:48:24 |
| Eccentricity: | 0.0003822 |
| inclination: | 51.6068° |
| perigee height: | 133 km |
| apogee height: | 138 km |
| right ascension of ascending node: | 355.5929° |
| argument of perigee: | 13.1809° |
| revolutions per day: | 16.51547366 |
| mean anomaly at epoch: | 68.7005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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