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 39440U 13066AA 23150.85384859 .00002952 00000-0 38407-3 0 9990
2 39440 97.7714 100.1741 0077339 83.7533 277.2481 14.79296252512791
| Epoch (UTC): | 30 May 2023 20:29:32 |
| Eccentricity: | 0.0077339 |
| inclination: | 97.7714° |
| perigee height: | 577 km |
| apogee height: | 686 km |
| right ascension of ascending node: | 100.1741° |
| argument of perigee: | 83.7533° |
| revolutions per day: | 14.79296252 |
| mean anomaly at epoch: | 277.2481° |
| orbit number at epoch: | 51279 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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