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 23028.53360012 .00000313 00000-0 11648-3 0 9992
2 27386 98.2126 4.4218 0001183 88.3316 21.1048 14.38230412 95814
| Epoch (UTC): | 28 January 2023 12:48:23 |
| Eccentricity: | 0.0001183 |
| inclination: | 98.2126° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 4.4218° |
| argument of perigee: | 88.3316° |
| revolutions per day: | 14.38230412 |
| mean anomaly at epoch: | 21.1048° |
| orbit number at epoch: | 9581 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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