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 23147.89229049 .00000195 00000-0 77568-4 0 9999
2 27386 98.2294 118.7300 0001280 89.4413 283.4022 14.38348133112971
| Epoch (UTC): | 27 May 2023 21:24:53 |
| Eccentricity: | 0.0001280 |
| inclination: | 98.2294° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 118.7300° |
| argument of perigee: | 89.4413° |
| revolutions per day: | 14.38348133 |
| mean anomaly at epoch: | 283.4022° |
| orbit number at epoch: | 11297 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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