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 40039U 14033AF 24337.55810024 .00006013 00000-0 59627-3 0 9993
2 40039 97.9170 264.7588 0012796 7.5450 352.5958 14.92106051567281
| Epoch (UTC): | 02 December 2024 13:23:39 |
| Eccentricity: | 0.0012796 |
| inclination: | 97.9170° |
| perigee height: | 582 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 264.7588° |
| argument of perigee: | 7.5450° |
| revolutions per day: | 14.92106051 |
| mean anomaly at epoch: | 352.5958° |
| orbit number at epoch: | 56728 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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