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 22225.85892361 .00005956 00000-0 11160-3 0 9992
2 25544 51.6422 50.8862 0005597 117.9700 82.2284 15.50167216354127
| Epoch (UTC): | 13 August 2022 20:36:51 |
| Eccentricity: | 0.0005597 |
| inclination: | 51.6422° |
| perigee height: | 412 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 50.8862° |
| argument of perigee: | 117.9700° |
| revolutions per day: | 15.50167216 |
| mean anomaly at epoch: | 82.2284° |
| orbit number at epoch: | 35412 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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