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 7530U 74089B 25082.99391955 -.00000010 00000-0 22643-3 0 9992
2 7530 101.9955 86.4273 0011885 270.2313 114.5888 12.53687474304344
| Epoch (UTC): | 23 March 2025 23:51:14 |
| Eccentricity: | 0.0011885 |
| inclination: | 101.9955° |
| perigee height: | 1440 km |
| apogee height: | 1458 km |
| right ascension of ascending node: | 86.4273° |
| argument of perigee: | 270.2313° |
| revolutions per day: | 12.53687474 |
| mean anomaly at epoch: | 114.5888° |
| orbit number at epoch: | 30434 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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