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 47951U 21022V 25157.62701764 .07883385 25648-5 89537-3 0 9993
2 47951 97.4004 72.1904 0010275 223.9924 136.0557 16.36879307233400
| Epoch (UTC): | 06 June 2025 15:02:54 |
| Eccentricity: | 0.0010275 |
| inclination: | 97.4004° |
| perigee height: | 167 km |
| apogee height: | 181 km |
| right ascension of ascending node: | 72.1904° |
| argument of perigee: | 223.9924° |
| revolutions per day: | 16.36879307 |
| mean anomaly at epoch: | 136.0557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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