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 14781U 84021B 23150.94136456 .00001281 00000-0 15675-3 0 9994
2 14781 97.6564 128.5418 0006555 256.5484 103.5001 14.84851968 91581
| Epoch (UTC): | 30 May 2023 22:35:33 |
| Eccentricity: | 0.0006555 |
| inclination: | 97.6564° |
| perigee height: | 609 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 128.5418° |
| argument of perigee: | 256.5484° |
| revolutions per day: | 14.84851968 |
| mean anomaly at epoch: | 103.5001° |
| orbit number at epoch: | 9158 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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