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 42427U 00055TX 22222.21612513 .00003405 00000-0 11701-2 0 9994
2 42427 98.9144 17.8358 0077798 146.0831 214.5362 14.35021242313081
| Epoch (UTC): | 10 August 2022 05:11:13 |
| Eccentricity: | 0.0077798 |
| inclination: | 98.9144° |
| perigee height: | 719 km |
| apogee height: | 830 km |
| right ascension of ascending node: | 17.8358° |
| argument of perigee: | 146.0831° |
| revolutions per day: | 14.35021242 |
| mean anomaly at epoch: | 214.5362° |
| orbit number at epoch: | 31308 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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