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 22148.90360635 .00000153 00000-0 63948-4 0 9999
2 27386 98.1823 130.9293 0001281 88.1823 330.8567 14.38126110 60722
| Epoch (UTC): | 28 May 2022 21:41:11 |
| Eccentricity: | 0.0001281 |
| inclination: | 98.1823° |
| perigee height: | 764 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 130.9293° |
| argument of perigee: | 88.1823° |
| revolutions per day: | 14.38126110 |
| mean anomaly at epoch: | 330.8567° |
| orbit number at epoch: | 6072 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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