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 00029U 60002B 22146.56903768 .00000356 00000-0 83512-4 0 9995
2 00029 48.3784 206.3440 0023730 20.9259 339.2619 14.74636940323036
| Epoch (UTC): | 26 May 2022 13:39:24 |
| Eccentricity: | 0.0023730 |
| inclination: | 48.3784° |
| perigee height: | 629 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 206.3440° |
| argument of perigee: | 20.9259° |
| revolutions per day: | 14.74636940 |
| mean anomaly at epoch: | 339.2619° |
| orbit number at epoch: | 32303 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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