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 22221.31834512 .00000255 00000-0 29705-3 0 9994
2 00005 34.2634 336.5046 1848132 275.4677 63.8983 10.84990872290287
| Epoch (UTC): | 09 August 2022 07:38:25 |
| Eccentricity: | 0.1848132 |
| inclination: | 34.2634° |
| perigee height: | 648 km |
| apogee height: | 3833 km |
| right ascension of ascending node: | 336.5046° |
| argument of perigee: | 275.4677° |
| revolutions per day: | 10.84990872 |
| mean anomaly at epoch: | 63.8983° |
| orbit number at epoch: | 29028 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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