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 27560U 02054B 23332.12052219 .00001399 00000-0 30374-3 0 9998
2 27560 98.4896 150.9137 0040298 26.0872 86.2306 14.59243792115143
| Epoch (UTC): | 28 November 2023 02:53:33 |
| Eccentricity: | 0.0040298 |
| inclination: | 98.4896° |
| perigee height: | 667 km |
| apogee height: | 724 km |
| right ascension of ascending node: | 150.9137° |
| argument of perigee: | 26.0872° |
| revolutions per day: | 14.59243792 |
| mean anomaly at epoch: | 86.2306° |
| orbit number at epoch: | 11514 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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