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 27601U 02056E 23334.83485309 .00000767 00000-0 28874-3 0 9996
2 27601 98.2089 317.0916 0072636 115.6662 308.0856 14.32555515 95226
| Epoch (UTC): | 30 November 2023 20:02:11 |
| Eccentricity: | 0.0072636 |
| inclination: | 98.2089° |
| perigee height: | 731 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 317.0916° |
| argument of perigee: | 115.6662° |
| revolutions per day: | 14.32555515 |
| mean anomaly at epoch: | 308.0856° |
| orbit number at epoch: | 9522 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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