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 40074U 14037F 24262.77749360 .00014878 00000-0 13158-2 0 9997
2 40074 98.3445 198.6096 0006932 109.7908 250.4059 14.96403846552768
| Epoch (UTC): | 18 September 2024 18:39:35 |
| Eccentricity: | 0.0006932 |
| inclination: | 98.3445° |
| perigee height: | 573 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 198.6096° |
| argument of perigee: | 109.7908° |
| revolutions per day: | 14.96403846 |
| mean anomaly at epoch: | 250.4059° |
| orbit number at epoch: | 55276 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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