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 23086.83993812 .00008729 00000-0 83230-3 0 9998
2 40042 98.0006 33.9133 0012695 187.4811 172.6220 14.93536635475898
| Epoch (UTC): | 27 March 2023 20:09:30 |
| Eccentricity: | 0.0012695 |
| inclination: | 98.0006° |
| perigee height: | 578 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 33.9133° |
| argument of perigee: | 187.4811° |
| revolutions per day: | 14.93536635 |
| mean anomaly at epoch: | 172.6220° |
| orbit number at epoch: | 47589 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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