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 22148.58364583 .00010373 00000-0 19118-3 0 9996
2 25544 51.6428 73.6809 0005012 167.7810 201.9879 15.49738929342146
| Epoch (UTC): | 28 May 2022 14:00:27 |
| Eccentricity: | 0.0005012 |
| inclination: | 51.6428° |
| perigee height: | 414 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 73.6809° |
| argument of perigee: | 167.7810° |
| revolutions per day: | 15.49738929 |
| mean anomaly at epoch: | 201.9879° |
| orbit number at epoch: | 34214 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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