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 22176.50304463 .00008726 00000-0 20857-3 0 9996
2 41465 97.0559 52.5774 0011670 101.4286 18.8033 15.41646121344773
| Epoch (UTC): | 25 June 2022 12:04:23 |
| Eccentricity: | 0.0011670 |
| inclination: | 97.0559° |
| perigee height: | 433 km |
| apogee height: | 449 km |
| right ascension of ascending node: | 52.5774° |
| argument of perigee: | 101.4286° |
| revolutions per day: | 15.41646121 |
| mean anomaly at epoch: | 18.8033° |
| orbit number at epoch: | 34477 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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