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 24259.56772203 .00020862 00000-0 18465-2 0 9998
2 40074 98.3431 195.1889 0006573 118.4290 241.7593 14.96292007552285
| Epoch (UTC): | 15 September 2024 13:37:31 |
| Eccentricity: | 0.0006573 |
| inclination: | 98.3431° |
| perigee height: | 574 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 195.1889° |
| argument of perigee: | 118.4290° |
| revolutions per day: | 14.96292007 |
| mean anomaly at epoch: | 241.7593° |
| orbit number at epoch: | 55228 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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