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 00022U 59009A 22274.53208375 .00003184 00000-0 24652-3 0 9995
2 00022 50.2816 134.5759 0133642 216.9501 142.2185 14.97490302595523
| Epoch (UTC): | 01 October 2022 12:46:12 |
| Eccentricity: | 0.0133642 |
| inclination: | 50.2816° |
| perigee height: | 482 km |
| apogee height: | 667 km |
| right ascension of ascending node: | 134.5759° |
| argument of perigee: | 216.9501° |
| revolutions per day: | 14.97490302 |
| mean anomaly at epoch: | 142.2185° |
| orbit number at epoch: | 59552 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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