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 22146.19628515 .00000361 00000-0 43703-3 0 9992
2 00005 34.2549 208.0143 1847417 297.3176 45.1330 10.84950623282128
| Epoch (UTC): | 26 May 2022 04:42:39 |
| Eccentricity: | 0.1847417 |
| inclination: | 34.2549° |
| perigee height: | 648 km |
| apogee height: | 3833 km |
| right ascension of ascending node: | 208.0143° |
| argument of perigee: | 297.3176° |
| revolutions per day: | 10.84950623 |
| mean anomaly at epoch: | 45.1330° |
| orbit number at epoch: | 28212 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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