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 41607U 16040J 22268.09047801 .00022596 00000-0 67298-3 0 9997
2 41607 97.2054 316.3656 0012059 121.1455 239.0973 15.34627999348040
| Epoch (UTC): | 25 September 2022 02:10:17 |
| Eccentricity: | 0.0012059 |
| inclination: | 97.2054° |
| perigee height: | 454 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 316.3656° |
| argument of perigee: | 121.1455° |
| revolutions per day: | 15.34627999 |
| mean anomaly at epoch: | 239.0973° |
| orbit number at epoch: | 34804 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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