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 23028.16662076 .00000347 00000-0 12772-3 0 9992
2 27386 98.2126 4.0708 0001181 88.3594 282.0984 14.38230289 95831
| Epoch (UTC): | 28 January 2023 03:59:56 |
| Eccentricity: | 0.0001181 |
| inclination: | 98.2126° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 4.0708° |
| argument of perigee: | 88.3594° |
| revolutions per day: | 14.38230289 |
| mean anomaly at epoch: | 282.0984° |
| orbit number at epoch: | 9583 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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