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 24357.83612206 .00009700 00000-0 10432-2 0 9993
2 39440 97.8328 298.0778 0066441 17.4369 342.9106 14.87090111596334
| Epoch (UTC): | 22 December 2024 20:04:00 |
| Eccentricity: | 0.0066441 |
| inclination: | 97.8328° |
| perigee height: | 560 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 298.0778° |
| argument of perigee: | 17.4369° |
| revolutions per day: | 14.87090111 |
| mean anomaly at epoch: | 342.9106° |
| orbit number at epoch: | 59633 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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