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 27875U 03040A 23266.32271372 -.00000273 00000-0 00000-0 0 9995
2 27875 8.3593 56.5348 0004716 122.2138 256.9479 1.00267177 22969
| Epoch (UTC): | 23 September 2023 07:44:42 |
| Eccentricity: | 0.0004716 |
| inclination: | 8.3593° |
| perigee height: | 35767 km |
| apogee height: | 35807 km |
| right ascension of ascending node: | 56.5348° |
| argument of perigee: | 122.2138° |
| revolutions per day: | 1.00267177 |
| mean anomaly at epoch: | 256.9479° |
| orbit number at epoch: | 2296 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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