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 22136.18268414 .00015873 00000-0 39074-3 0 9993
2 41465 97.0607 13.6186 0007959 243.0517 234.1016 15.40644100338565
| Epoch (UTC): | 16 May 2022 04:23:03 |
| Eccentricity: | 0.0007959 |
| inclination: | 97.0607° |
| perigee height: | 439 km |
| apogee height: | 449 km |
| right ascension of ascending node: | 13.6186° |
| argument of perigee: | 243.0517° |
| revolutions per day: | 15.40644100 |
| mean anomaly at epoch: | 234.1016° |
| orbit number at epoch: | 33856 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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