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 41604U 16040F 22267.56380513 .00004470 00000-0 18176-3 0 9997
2 41604 97.2020 308.2355 0012785 136.7735 223.4509 15.24953351347566
| Epoch (UTC): | 24 September 2022 13:31:52 |
| Eccentricity: | 0.0012785 |
| inclination: | 97.2020° |
| perigee height: | 482 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 308.2355° |
| argument of perigee: | 136.7735° |
| revolutions per day: | 15.24953351 |
| mean anomaly at epoch: | 223.4509° |
| orbit number at epoch: | 34756 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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