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 22027.51174303 .00007551 00000-0 14174-3 0 9995
2 25544 51.6451 313.2440 0006867 67.2904 104.2189 15.49665136323364
| Epoch (UTC): | 27 January 2022 12:16:54 |
| Eccentricity: | 0.0006867 |
| inclination: | 51.6451° |
| perigee height: | 413 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 313.2440° |
| argument of perigee: | 67.2904° |
| revolutions per day: | 15.49665136 |
| mean anomaly at epoch: | 104.2189° |
| orbit number at epoch: | 32336 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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