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 23039.52582803 .00000460 00000-0 16511-3 0 9994
2 27386 98.2148 14.9356 0001220 89.5281 20.6565 14.38238756 97395
| Epoch (UTC): | 08 February 2023 12:37:11 |
| Eccentricity: | 0.0001220 |
| inclination: | 98.2148° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 14.9356° |
| argument of perigee: | 89.5281° |
| revolutions per day: | 14.38238756 |
| mean anomaly at epoch: | 20.6565° |
| orbit number at epoch: | 9739 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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