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 39430U 13066Q 23332.62269673 .00003426 00000-0 58740-3 0 9991
2 39430 97.7566 214.0664 0143188 172.1186 188.2315 14.62800435533388
| Epoch (UTC): | 28 November 2023 14:56:40 |
| Eccentricity: | 0.0143188 |
| inclination: | 97.7566° |
| perigee height: | 583 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 214.0664° |
| argument of perigee: | 172.1186° |
| revolutions per day: | 14.62800435 |
| mean anomaly at epoch: | 188.2315° |
| orbit number at epoch: | 53338 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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