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 22179.94406266 .00010016 00000-0 23853-3 0 9995
2 41465 97.0560 55.9044 0011617 90.0867 35.4826 15.41718940345305
| Epoch (UTC): | 28 June 2022 22:39:27 |
| Eccentricity: | 0.0011617 |
| inclination: | 97.0560° |
| perigee height: | 433 km |
| apogee height: | 449 km |
| right ascension of ascending node: | 55.9044° |
| argument of perigee: | 90.0867° |
| revolutions per day: | 15.41718940 |
| mean anomaly at epoch: | 35.4826° |
| orbit number at epoch: | 34530 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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