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 40907U 15049J 23153.70423844 .00013819 00000-0 50773-3 0 9992
2 40907 97.4909 161.2908 0010371 194.6911 165.4028 15.27983024426278
| Epoch (UTC): | 02 June 2023 16:54:06 |
| Eccentricity: | 0.0010371 |
| inclination: | 97.4909° |
| perigee height: | 475 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 161.2908° |
| argument of perigee: | 194.6911° |
| revolutions per day: | 15.27983024 |
| mean anomaly at epoch: | 165.4028° |
| orbit number at epoch: | 42627 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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