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 24357.90134160 .00014693 00000-0 10210-2 0 9996
2 40025 98.0669 325.9072 0009134 267.3924 92.6255 15.05610010571213
| Epoch (UTC): | 22 December 2024 21:37:55 |
| Eccentricity: | 0.0009134 |
| inclination: | 98.0669° |
| perigee height: | 543 km |
| apogee height: | 556 km |
| right ascension of ascending node: | 325.9072° |
| argument of perigee: | 267.3924° |
| revolutions per day: | 15.05610010 |
| mean anomaly at epoch: | 92.6255° |
| orbit number at epoch: | 57121 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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