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 41038U 15069A 24358.16244741 .00001108 00000-0 14556-3 0 9992
2 41038 98.0471 13.6663 0001736 32.2678 327.8641 14.82262405490454
| Epoch (UTC): | 23 December 2024 03:53:55 |
| Eccentricity: | 0.0001736 |
| inclination: | 98.0471° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 13.6663° |
| argument of perigee: | 32.2678° |
| revolutions per day: | 14.82262405 |
| mean anomaly at epoch: | 327.8641° |
| orbit number at epoch: | 49045 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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