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 22137.20562086 .00000229 00000-0 89223-4 0 9992
2 27386 98.1821 119.7816 0001306 85.9431 285.0137 14.38118978 59044
| Epoch (UTC): | 17 May 2022 04:56:05 |
| Eccentricity: | 0.0001306 |
| inclination: | 98.1821° |
| perigee height: | 764 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 119.7816° |
| argument of perigee: | 85.9431° |
| revolutions per day: | 14.38118978 |
| mean anomaly at epoch: | 285.0137° |
| orbit number at epoch: | 5904 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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