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 39446U 13066AG 24260.84840120 .00010676 00000-0 11405-2 0 9996
2 39446 97.7872 208.7431 0056224 278.3553 81.1291 14.87796170582327
| Epoch (UTC): | 16 September 2024 20:21:41 |
| Eccentricity: | 0.0056224 |
| inclination: | 97.7872° |
| perigee height: | 565 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 208.7431° |
| argument of perigee: | 278.3553° |
| revolutions per day: | 14.87796170 |
| mean anomaly at epoch: | 81.1291° |
| orbit number at epoch: | 58232 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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