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 47688U 21006EP 22176.67117626 .00003929 00000-0 20634-3 0 9997
2 47688 97.4438 235.3077 0009170 233.4475 126.5915 15.16257192 79455
| Epoch (UTC): | 25 June 2022 16:06:29 |
| Eccentricity: | 0.0009170 |
| inclination: | 97.4438° |
| perigee height: | 511 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 235.3077° |
| argument of perigee: | 233.4475° |
| revolutions per day: | 15.16257192 |
| mean anomaly at epoch: | 126.5915° |
| orbit number at epoch: | 7945 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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