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 22145.97005428 .00000321 00000-0 11940-3 0 9990
2 27386 98.1807 128.1300 0000888 65.4232 294.7111 14.38125293 60304
| Epoch (UTC): | 25 May 2022 23:16:52 |
| Eccentricity: | 0.0000888 |
| inclination: | 98.1807° |
| perigee height: | 764 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 128.1300° |
| argument of perigee: | 65.4232° |
| revolutions per day: | 14.38125293 |
| mean anomaly at epoch: | 294.7111° |
| orbit number at epoch: | 6030 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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