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 22178.40823120 .00001737 00000-0 18325-3 0 9991
2 40042 97.9712 117.0885 0015089 22.4947 337.6928 14.90567960435139
| Epoch (UTC): | 27 June 2022 09:47:51 |
| Eccentricity: | 0.0015089 |
| inclination: | 97.9712° |
| perigee height: | 585 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 117.0885° |
| argument of perigee: | 22.4947° |
| revolutions per day: | 14.90567960 |
| mean anomaly at epoch: | 337.6928° |
| orbit number at epoch: | 43513 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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