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 29U 60002B 24257.17398300 .00004897 00000-0 71702-3 0 9998
2 29 48.3767 192.1805 0022878 24.9745 335.2270 14.76802247447279
| Epoch (UTC): | 13 September 2024 04:10:32 |
| Eccentricity: | 0.0022878 |
| inclination: | 48.3767° |
| perigee height: | 623 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 192.1805° |
| argument of perigee: | 24.9745° |
| revolutions per day: | 14.76802247 |
| mean anomaly at epoch: | 335.2270° |
| orbit number at epoch: | 44727 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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