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 40910U 15049M 23151.39082735 .00025813 00000-0 71678-3 0 9993
2 40910 97.4621 164.2742 0010485 170.4964 189.6480 15.36821356426301
| Epoch (UTC): | 31 May 2023 09:22:47 |
| Eccentricity: | 0.0010485 |
| inclination: | 97.4621° |
| perigee height: | 448 km |
| apogee height: | 462 km |
| right ascension of ascending node: | 164.2742° |
| argument of perigee: | 170.4964° |
| revolutions per day: | 15.36821356 |
| mean anomaly at epoch: | 189.6480° |
| orbit number at epoch: | 42630 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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