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 23028.93376789 .00000293 00000-0 10989-3 0 9998
2 27386 98.2126 4.8044 0001188 88.4188 291.7337 14.38230608 95877
| Epoch (UTC): | 28 January 2023 22:24:37 |
| Eccentricity: | 0.0001188 |
| inclination: | 98.2126° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 4.8044° |
| argument of perigee: | 88.4188° |
| revolutions per day: | 14.38230608 |
| mean anomaly at epoch: | 291.7337° |
| orbit number at epoch: | 9587 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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