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 40042U 14033AJ 25200.48397265 .00008966 00000-0 42609-3 0 9997
2 40042 98.1041 193.6725 0008702 212.3683 147.7017 15.19445619602842
| Epoch (UTC): | 19 July 2025 11:36:55 |
| Eccentricity: | 0.0008702 |
| inclination: | 98.1041° |
| perigee height: | 501 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 193.6725° |
| argument of perigee: | 212.3683° |
| revolutions per day: | 15.19445619 |
| mean anomaly at epoch: | 147.7017° |
| orbit number at epoch: | 60284 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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