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 23090.12269240 .00012466 00000-0 11833-2 0 9998
2 40042 98.0007 37.2533 0013143 175.7243 184.4090 14.93606930476891
| Epoch (UTC): | 31 March 2023 02:56:40 |
| Eccentricity: | 0.0013143 |
| inclination: | 98.0007° |
| perigee height: | 577 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 37.2533° |
| argument of perigee: | 175.7243° |
| revolutions per day: | 14.93606930 |
| mean anomaly at epoch: | 184.4090° |
| orbit number at epoch: | 47689 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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