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 22177.15829770 .00010477 00000-0 24987-3 0 9995
2 41465 97.0561 53.2106 0011539 98.5484 55.9358 15.41664974344872
| Epoch (UTC): | 26 June 2022 03:47:56 |
| Eccentricity: | 0.0011539 |
| inclination: | 97.0561° |
| perigee height: | 433 km |
| apogee height: | 449 km |
| right ascension of ascending node: | 53.2106° |
| argument of perigee: | 98.5484° |
| revolutions per day: | 15.41664974 |
| mean anomaly at epoch: | 55.9358° |
| orbit number at epoch: | 34487 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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