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 23151.41211529 .00012494 00000-0 46035-3 0 9997
2 40907 97.4915 158.9864 0010057 202.8502 157.2291 15.27918534425924
| Epoch (UTC): | 31 May 2023 09:53:26 |
| Eccentricity: | 0.0010057 |
| inclination: | 97.4915° |
| perigee height: | 475 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 158.9864° |
| argument of perigee: | 202.8502° |
| revolutions per day: | 15.27918534 |
| mean anomaly at epoch: | 157.2291° |
| orbit number at epoch: | 42592 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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