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 22179.81795130 .00001268 00000-0 13535-3 0 9993
2 40042 97.9712 118.5113 0014946 18.0502 342.1243 14.90571200435344
| Epoch (UTC): | 28 June 2022 19:37:50 |
| Eccentricity: | 0.0014946 |
| inclination: | 97.9712° |
| perigee height: | 586 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 118.5113° |
| argument of perigee: | 18.0502° |
| revolutions per day: | 14.90571200 |
| mean anomaly at epoch: | 342.1243° |
| orbit number at epoch: | 43534 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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