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 27386U 02009A 22334.40671417 .00000130 00000-0 56467-4 0 9997
2 27386 98.2052 307.9049 0001318 85.3348 69.8746 14.38190574 87311
| Epoch (UTC): | 30 November 2022 09:45:40 |
| Eccentricity: | 0.0001318 |
| inclination: | 98.2052° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 307.9049° |
| argument of perigee: | 85.3348° |
| revolutions per day: | 14.38190574 |
| mean anomaly at epoch: | 69.8746° |
| orbit number at epoch: | 8731 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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