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 22136.21862646 .00011440 00000-0 21209-3 0 9996
2 25544 51.6405 134.9015 0005204 123.9413 341.3931 15.49453276340221
| Epoch (UTC): | 16 May 2022 05:14:49 |
| Eccentricity: | 0.0005204 |
| inclination: | 51.6405° |
| perigee height: | 415 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 134.9015° |
| argument of perigee: | 123.9413° |
| revolutions per day: | 15.49453276 |
| mean anomaly at epoch: | 341.3931° |
| orbit number at epoch: | 34022 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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