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 25544U 98067A 22184.32460500 .00005934 00000-0 11261-3 0 9992
2 25544 51.6431 256.6653 0004465 326.5711 149.3182 15.49807134347687
| Epoch (UTC): | 03 July 2022 07:47:25 |
| Eccentricity: | 0.0004465 |
| inclination: | 51.6431° |
| perigee height: | 414 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 256.6653° |
| argument of perigee: | 326.5711° |
| revolutions per day: | 15.49807134 |
| mean anomaly at epoch: | 149.3182° |
| orbit number at epoch: | 34768 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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