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 23033.54301775 .00000240 00000-0 92427-4 0 9994
2 27386 98.2133 9.2128 0001225 88.9816 22.3175 14.38233515 96534
| Epoch (UTC): | 02 February 2023 13:01:56 |
| Eccentricity: | 0.0001225 |
| inclination: | 98.2133° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 9.2128° |
| argument of perigee: | 88.9816° |
| revolutions per day: | 14.38233515 |
| mean anomaly at epoch: | 22.3175° |
| orbit number at epoch: | 9653 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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