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 41465U 16026B 24106.13728541 .23005584 23685-5 20852-3 0 9995
2 41465 96.9058 342.9388 0009939 249.4867 270.8904 16.51426536447606
| Epoch (UTC): | 15 April 2024 03:17:41 |
| Eccentricity: | 0.0009939 |
| inclination: | 96.9058° |
| perigee height: | 129 km |
| apogee height: | 142 km |
| right ascension of ascending node: | 342.9388° |
| argument of perigee: | 249.4867° |
| revolutions per day: | 16.51426536 |
| mean anomaly at epoch: | 270.8904° |
| orbit number at epoch: | 44760 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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