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 35943U 09054B 25348.19350067 .00000042 00000-0 00000-0 0 9991
2 35943 0.0220 326.3385 0002973 309.6622 299.8034 1.00269903 59446
| Epoch (UTC): | 14 December 2025 04:38:38 |
| Eccentricity: | 0.0002973 |
| inclination: | 0.0220° |
| perigee height: | 35774 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 326.3385° |
| argument of perigee: | 309.6622° |
| revolutions per day: | 1.00269903 |
| mean anomaly at epoch: | 299.8034° |
| orbit number at epoch: | 5944 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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