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 22140.92025341 .00017688 00000-0 43268-3 0 9996
2 41465 97.0594 18.1938 0008161 223.9808 233.4491 15.40812590339291
| Epoch (UTC): | 20 May 2022 22:05:09 |
| Eccentricity: | 0.0008161 |
| inclination: | 97.0594° |
| perigee height: | 438 km |
| apogee height: | 449 km |
| right ascension of ascending node: | 18.1938° |
| argument of perigee: | 223.9808° |
| revolutions per day: | 15.40812590 |
| mean anomaly at epoch: | 233.4491° |
| orbit number at epoch: | 33929 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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