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 23087.52786684 .00000525 00000-0 18620-3 0 9995
2 27386 98.2230 60.8812 0001405 86.3873 22.6930 14.38298041104290
| Epoch (UTC): | 28 March 2023 12:40:07 |
| Eccentricity: | 0.0001405 |
| inclination: | 98.2230° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 60.8812° |
| argument of perigee: | 86.3873° |
| revolutions per day: | 14.38298041 |
| mean anomaly at epoch: | 22.6930° |
| orbit number at epoch: | 10429 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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