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 25732U 99025C 23159.56687706 .00000074 00000-0 57830-4 0 9997
2 25732 98.8036 203.8975 0037069 350.8494 129.7928 14.17825305245855
| Epoch (UTC): | 08 June 2023 13:36:18 |
| Eccentricity: | 0.0037069 |
| inclination: | 98.8036° |
| perigee height: | 806 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 203.8975° |
| argument of perigee: | 350.8494° |
| revolutions per day: | 14.17825305 |
| mean anomaly at epoch: | 129.7928° |
| orbit number at epoch: | 24585 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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