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 22221.71184699 .00000179 00000-0 57157-4 0 9999
2 00029 48.3782 211.5493 0024260 342.5502 17.4574 14.74694946334120
| Epoch (UTC): | 09 August 2022 17:05:03 |
| Eccentricity: | 0.0024260 |
| inclination: | 48.3782° |
| perigee height: | 629 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 211.5493° |
| argument of perigee: | 342.5502° |
| revolutions per day: | 14.74694946 |
| mean anomaly at epoch: | 17.4574° |
| orbit number at epoch: | 33412 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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