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 10541U 77123B 24357.85028312 .00000103 00000-0 67671-4 0 9996
2 10541 75.8344 196.9014 0299205 276.6451 80.0718 13.89201070381302
| Epoch (UTC): | 22 December 2024 20:24:24 |
| Eccentricity: | 0.0299205 |
| inclination: | 75.8344° |
| perigee height: | 713 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 196.9014° |
| argument of perigee: | 276.6451° |
| revolutions per day: | 13.89201070 |
| mean anomaly at epoch: | 80.0718° |
| orbit number at epoch: | 38130 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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