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 23270.75787800 .00003138 00000-0 34303-3 0 9994
2 40039 97.8915 192.9882 0013301 350.0150 10.0800 14.88520824502983
| Epoch (UTC): | 27 September 2023 18:11:20 |
| Eccentricity: | 0.0013301 |
| inclination: | 97.8915° |
| perigee height: | 593 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 192.9882° |
| argument of perigee: | 350.0150° |
| revolutions per day: | 14.88520824 |
| mean anomaly at epoch: | 10.0800° |
| orbit number at epoch: | 50298 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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