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 42017U 17008BX 22182.71193032 .00006805 00000-0 20267-3 0 9990
2 42017 97.2678 248.6215 0005464 174.6375 185.4928 15.35002556299262
| Epoch (UTC): | 01 July 2022 17:05:10 |
| Eccentricity: | 0.0005464 |
| inclination: | 97.2678° |
| perigee height: | 457 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 248.6215° |
| argument of perigee: | 174.6375° |
| revolutions per day: | 15.35002556 |
| mean anomaly at epoch: | 185.4928° |
| orbit number at epoch: | 29926 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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