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 27561U 02054C 22227.76180974 .00000261 00000-0 69427-4 0 9990
2 27561 98.5087 36.7305 0046970 123.9502 236.6173 14.56128638 46554
| Epoch (UTC): | 15 August 2022 18:17:00 |
| Eccentricity: | 0.0046970 |
| inclination: | 98.5087° |
| perigee height: | 672 km |
| apogee height: | 739 km |
| right ascension of ascending node: | 36.7305° |
| argument of perigee: | 123.9502° |
| revolutions per day: | 14.56128638 |
| mean anomaly at epoch: | 236.6173° |
| orbit number at epoch: | 4655 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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