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 40042U 14033AJ 22135.77764059 .00004834 00000-0 50228-3 0 9998
2 40042 97.9700 74.0772 0015088 150.3508 209.8567 14.90309163428787
| Epoch (UTC): | 15 May 2022 18:39:48 |
| Eccentricity: | 0.0015088 |
| inclination: | 97.9700° |
| perigee height: | 586 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 74.0772° |
| argument of perigee: | 150.3508° |
| revolutions per day: | 14.90309163 |
| mean anomaly at epoch: | 209.8567° |
| orbit number at epoch: | 42878 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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