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 24258.89713520 .00016493 00000-0 12570-2 0 9998
2 40025 98.0534 222.7747 0010049 223.7550 136.2878 15.02090135556334
| Epoch (UTC): | 14 September 2024 21:31:52 |
| Eccentricity: | 0.0010049 |
| inclination: | 98.0534° |
| perigee height: | 553 km |
| apogee height: | 567 km |
| right ascension of ascending node: | 222.7747° |
| argument of perigee: | 223.7550° |
| revolutions per day: | 15.02090135 |
| mean anomaly at epoch: | 136.2878° |
| orbit number at epoch: | 55633 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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