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 4679U 70025BC 22269.50012649 .00000234 00000-0 33854-3 0 9993
2 4679 100.0712 5.6455 0017841 30.0550 342.7409 13.66731374604828
| Epoch (UTC): | 26 September 2022 12:00:10 |
| Eccentricity: | 0.0017841 |
| inclination: | 100.0712° |
| perigee height: | 998 km |
| apogee height: | 1024 km |
| right ascension of ascending node: | 5.6455° |
| argument of perigee: | 30.0550° |
| revolutions per day: | 13.66731374 |
| mean anomaly at epoch: | 342.7409° |
| orbit number at epoch: | 60482 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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