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 22145.27545001 .00000387 00000-0 46771-3 0 9994
2 00005 34.2553 210.8511 1847468 293.1756 48.5123 10.84950011282024
| Epoch (UTC): | 25 May 2022 06:36:38 |
| Eccentricity: | 0.1847468 |
| inclination: | 34.2553° |
| perigee height: | 648 km |
| apogee height: | 3833 km |
| right ascension of ascending node: | 210.8511° |
| argument of perigee: | 293.1756° |
| revolutions per day: | 10.84950011 |
| mean anomaly at epoch: | 48.5123° |
| orbit number at epoch: | 28202 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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