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 24259.64888926 .00029442 00000-0 68702-3 0 9996
2 41604 97.1186 285.7004 0010085 84.2569 275.9829 15.42119680458100
| Epoch (UTC): | 15 September 2024 15:34:24 |
| Eccentricity: | 0.0010085 |
| inclination: | 97.1186° |
| perigee height: | 433 km |
| apogee height: | 447 km |
| right ascension of ascending node: | 285.7004° |
| argument of perigee: | 84.2569° |
| revolutions per day: | 15.42119680 |
| mean anomaly at epoch: | 275.9829° |
| orbit number at epoch: | 45810 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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