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 22219.40813307 .00000056 00000-0 39027-4 0 9997
2 00029 48.3780 222.4273 0024340 332.7700 27.1935 14.74692786333785
| Epoch (UTC): | 07 August 2022 09:47:42 |
| Eccentricity: | 0.0024340 |
| inclination: | 48.3780° |
| perigee height: | 629 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 222.4273° |
| argument of perigee: | 332.7700° |
| revolutions per day: | 14.74692786 |
| mean anomaly at epoch: | 27.1935° |
| orbit number at epoch: | 33378 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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