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 27431U 02024B 25140.92575579 .00000066 00000-0 62812-4 0 9991
2 27431 99.0061 186.8364 0014329 265.2425 94.7109 14.10142474184264
| Epoch (UTC): | 20 May 2025 22:13:05 |
| Eccentricity: | 0.0014329 |
| inclination: | 99.0061° |
| perigee height: | 848 km |
| apogee height: | 869 km |
| right ascension of ascending node: | 186.8364° |
| argument of perigee: | 265.2425° |
| revolutions per day: | 14.10142474 |
| mean anomaly at epoch: | 94.7109° |
| orbit number at epoch: | 18426 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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