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 22148.53404431 .00000288 00000-0 73347-4 0 9996
2 00029 48.3782 197.0663 0023655 29.4029 330.8208 14.74638988323329
| Epoch (UTC): | 28 May 2022 12:49:01 |
| Eccentricity: | 0.0023655 |
| inclination: | 48.3782° |
| perigee height: | 629 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 197.0663° |
| argument of perigee: | 29.4029° |
| revolutions per day: | 14.74638988 |
| mean anomaly at epoch: | 330.8208° |
| orbit number at epoch: | 32332 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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