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 00047U 60007C 22146.48658997 .00000329 00000-0 98609-4 0 9995
2 00047 66.6670 61.5658 0222691 146.8959 214.6314 14.42331664236779
| Epoch (UTC): | 26 May 2022 11:40:41 |
| Eccentricity: | 0.0222691 |
| inclination: | 66.6670° |
| perigee height: | 592 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 61.5658° |
| argument of perigee: | 146.8959° |
| revolutions per day: | 14.42331664 |
| mean anomaly at epoch: | 214.6314° |
| orbit number at epoch: | 23677 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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