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 40922U 15050C 23332.54509038 .00000011 00000-0 94754-5 0 9991
2 40922 82.4852 298.5838 0014835 270.8171 89.1209 12.42888707371140
| Epoch (UTC): | 28 November 2023 13:04:55 |
| Eccentricity: | 0.0014835 |
| inclination: | 82.4852° |
| perigee height: | 1482 km |
| apogee height: | 1506 km |
| right ascension of ascending node: | 298.5838° |
| argument of perigee: | 270.8171° |
| revolutions per day: | 12.42888707 |
| mean anomaly at epoch: | 89.1209° |
| orbit number at epoch: | 37114 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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