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 22148.15080520 .00000317 00000-0 95905-4 0 9995
2 00047 66.6673 57.1150 0222568 145.6529 215.9199 14.42333183237014
| Epoch (UTC): | 28 May 2022 03:37:09 |
| Eccentricity: | 0.0222568 |
| inclination: | 66.6673° |
| perigee height: | 592 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 57.1150° |
| argument of perigee: | 145.6529° |
| revolutions per day: | 14.42333183 |
| mean anomaly at epoch: | 215.9199° |
| orbit number at epoch: | 23701 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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