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 20442U 90005G 22135.84389223 .00000161 00000-0 75670-4 0 9995
2 20442 98.7916 100.2119 0010590 264.4548 95.5427 14.33053257688496
| Epoch (UTC): | 15 May 2022 20:15:12 |
| Eccentricity: | 0.0010590 |
| inclination: | 98.7916° |
| perigee height: | 774 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 100.2119° |
| argument of perigee: | 264.4548° |
| revolutions per day: | 14.33053257 |
| mean anomaly at epoch: | 95.5427° |
| orbit number at epoch: | 68849 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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