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 23266.71579292 .00010782 00000-0 36265-3 0 9990
2 41604 97.1567 298.8318 0008214 290.5373 69.4987 15.30939171403161
Epoch (UTC): | 23 September 2023 17:10:44 |
Eccentricity: | 0.0008214 |
inclination: | 97.1567° |
perigee height: | 467 km |
apogee height: | 478 km |
right ascension of ascending node: | 298.8318° |
argument of perigee: | 290.5373° |
revolutions per day: | 15.30939171 |
mean anomaly at epoch: | 69.4987° |
orbit number at epoch: | 40316 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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