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 47963U 21022AH 23202.53360687 .17381218 26597-5 10224-2 0 9999
2 47963 97.4716 114.0875 0012162 215.2271 144.8226 16.40939998128010
| Epoch (UTC): | 21 July 2023 12:48:23 |
| Eccentricity: | 0.0012162 |
| inclination: | 97.4716° |
| perigee height: | 155 km |
| apogee height: | 171 km |
| right ascension of ascending node: | 114.0875° |
| argument of perigee: | 215.2271° |
| revolutions per day: | 16.40939998 |
| mean anomaly at epoch: | 144.8226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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