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 20323U 89089B 25193.90848074 .00000159 00000-0 48326-4 0 9996
2 20323 97.1010 74.1868 0069744 158.8603 201.5502 14.50411898860971
| Epoch (UTC): | 12 July 2025 21:48:12 |
| Eccentricity: | 0.0069744 |
| inclination: | 97.1010° |
| perigee height: | 675 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 74.1868° |
| argument of perigee: | 158.8603° |
| revolutions per day: | 14.50411898 |
| mean anomaly at epoch: | 201.5502° |
| orbit number at epoch: | 86097 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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