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 10096U 77055B 22143.86721670 .00000610 00000-0 66075-4 0 9994
2 10096 75.8362 38.8583 0042856 295.6403 64.0363 14.88944251430137
| Epoch (UTC): | 23 May 2022 20:48:47 |
| Eccentricity: | 0.0042856 |
| inclination: | 75.8362° |
| perigee height: | 571 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 38.8583° |
| argument of perigee: | 295.6403° |
| revolutions per day: | 14.88944251 |
| mean anomaly at epoch: | 64.0363° |
| orbit number at epoch: | 43013 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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