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 22177.40128587 .00002227 00000-0 23325-3 0 9996
2 40042 97.9710 116.0722 0015187 25.7848 334.4123 14.90565333434987
| Epoch (UTC): | 26 June 2022 09:37:51 |
| Eccentricity: | 0.0015187 |
| inclination: | 97.9710° |
| perigee height: | 585 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 116.0722° |
| argument of perigee: | 25.7848° |
| revolutions per day: | 14.90565333 |
| mean anomaly at epoch: | 334.4123° |
| orbit number at epoch: | 43498 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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