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 12227U 78026BU 24357.88256398 .00012424 00000-0 12465-2 0 9990
2 12227 98.7517 122.0861 0076757 155.2467 205.2462 14.89277313319082
| Epoch (UTC): | 22 December 2024 21:10:53 |
| Eccentricity: | 0.0076757 |
| inclination: | 98.7517° |
| perigee height: | 546 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 122.0861° |
| argument of perigee: | 155.2467° |
| revolutions per day: | 14.89277313 |
| mean anomaly at epoch: | 205.2462° |
| orbit number at epoch: | 31908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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