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 24282.35091188 .00098556 00000-0 21709-2 0 9993
2 41604 97.1159 307.8743 0007679 13.2179 346.9269 15.43546748461606
| Epoch (UTC): | 08 October 2024 08:25:18 |
| Eccentricity: | 0.0007679 |
| inclination: | 97.1159° |
| perigee height: | 430 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 307.8743° |
| argument of perigee: | 13.2179° |
| revolutions per day: | 15.43546748 |
| mean anomaly at epoch: | 346.9269° |
| orbit number at epoch: | 46160 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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