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 32953U 08025A 23153.71775314 .00000041 00000-0 22270-3 0 9997
2 32953 82.5019 326.0974 0019109 213.9035 146.0824 12.43124592681859
| Epoch (UTC): | 02 June 2023 17:13:33 |
| Eccentricity: | 0.0019109 |
| inclination: | 82.5019° |
| perigee height: | 1478 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 326.0974° |
| argument of perigee: | 213.9035° |
| revolutions per day: | 12.43124592 |
| mean anomaly at epoch: | 146.0824° |
| orbit number at epoch: | 68185 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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