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 22176.53457065 .00000084 00000-0 41287-4 0 9998
2 27386 98.1834 157.2632 0001321 89.6892 19.0675 14.38134322 64690
| Epoch (UTC): | 25 June 2022 12:49:46 |
| Eccentricity: | 0.0001321 |
| inclination: | 98.1834° |
| perigee height: | 764 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 157.2632° |
| argument of perigee: | 89.6892° |
| revolutions per day: | 14.38134322 |
| mean anomaly at epoch: | 19.0675° |
| orbit number at epoch: | 6469 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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