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 26905U 01040A 24241.79499277 0.00000600 00000-0 36656-3 0 02
2 26905 63.3771 140.7930 0601213 8.0861 351.9139 13.41198276 04
| Epoch (UTC): | 28 August 2024 19:04:47 |
| Eccentricity: | 0.0601213 |
| inclination: | 63.3771° |
| perigee height: | 655 km |
| apogee height: | 1555 km |
| right ascension of ascending node: | 140.7930° |
| argument of perigee: | 8.0861° |
| revolutions per day: | 13.41198276 |
| mean anomaly at epoch: | 351.9139° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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