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 41465U 16026B 23342.15002494 .00045383 00000-0 34069-3 0 9992
2 41465 96.9652 211.5146 0003247 325.4556 34.6497 15.72476151427156
| Epoch (UTC): | 08 December 2023 03:36:02 |
| Eccentricity: | 0.0003247 |
| inclination: | 96.9652° |
| perigee height: | 349 km |
| apogee height: | 354 km |
| right ascension of ascending node: | 211.5146° |
| argument of perigee: | 325.4556° |
| revolutions per day: | 15.72476151 |
| mean anomaly at epoch: | 34.6497° |
| orbit number at epoch: | 42715 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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