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 29093U 06015B 22148.53322945 .00031554 00000-0 40531-3 0 9999
2 29093 97.6041 6.7504 0038539 255.7720 103.9253 15.58141336896553
| Epoch (UTC): | 28 May 2022 12:47:51 |
| Eccentricity: | 0.0038539 |
| inclination: | 97.6041° |
| perigee height: | 367 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 6.7504° |
| argument of perigee: | 255.7720° |
| revolutions per day: | 15.58141336 |
| mean anomaly at epoch: | 103.9253° |
| orbit number at epoch: | 89655 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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