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 27422U 02021B 22222.27581503 .00000100 00000-0 55712-4 0 9998
2 27422 98.4513 166.6643 0013449 78.7378 281.5315 14.29435200 55243
| Epoch (UTC): | 10 August 2022 06:37:10 |
| Eccentricity: | 0.0013449 |
| inclination: | 98.4513° |
| perigee height: | 784 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 166.6643° |
| argument of perigee: | 78.7378° |
| revolutions per day: | 14.29435200 |
| mean anomaly at epoch: | 281.5315° |
| orbit number at epoch: | 5524 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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