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 00005U 58002B 22220.67386553 .00000252 00000-0 29159-3 0 9999
2 00005 34.2631 338.4901 1848133 272.5686 66.5811 10.84990561290212
| Epoch (UTC): | 08 August 2022 16:10:21 |
| Eccentricity: | 0.1848133 |
| inclination: | 34.2631° |
| perigee height: | 648 km |
| apogee height: | 3833 km |
| right ascension of ascending node: | 338.4901° |
| argument of perigee: | 272.5686° |
| revolutions per day: | 10.84990561 |
| mean anomaly at epoch: | 66.5811° |
| orbit number at epoch: | 29021 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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