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 40025U 14033R 24259.89635253 .00017777 00000-0 13530-2 0 9998
2 40025 98.0535 223.8121 0010153 219.6202 140.4280 15.02123619556997
| Epoch (UTC): | 15 September 2024 21:30:44 |
| Eccentricity: | 0.0010153 |
| inclination: | 98.0535° |
| perigee height: | 553 km |
| apogee height: | 567 km |
| right ascension of ascending node: | 223.8121° |
| argument of perigee: | 219.6202° |
| revolutions per day: | 15.02123619 |
| mean anomaly at epoch: | 140.4280° |
| orbit number at epoch: | 55699 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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