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 22221.88245056 .00000066 00000-0 35269-4 0 9995
2 27386 98.1871 200.4943 0001383 85.6454 306.1815 14.38143715 71213
| Epoch (UTC): | 09 August 2022 21:10:43 |
| Eccentricity: | 0.0001383 |
| inclination: | 98.1871° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 200.4943° |
| argument of perigee: | 85.6454° |
| revolutions per day: | 14.38143715 |
| mean anomaly at epoch: | 306.1815° |
| orbit number at epoch: | 7121 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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