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 23032.56948006 .00000234 00000-0 90473-4 0 9991
2 27386 98.2131 8.2816 0001214 88.7371 24.8642 14.38232883 96462
| Epoch (UTC): | 01 February 2023 13:40:03 |
| Eccentricity: | 0.0001214 |
| inclination: | 98.2131° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 8.2816° |
| argument of perigee: | 88.7371° |
| revolutions per day: | 14.38232883 |
| mean anomaly at epoch: | 24.8642° |
| orbit number at epoch: | 9646 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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