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 39195U 13032B 24357.86782803 .00034678 00000-0 41481-3 0 9998
2 39195 74.7210 266.8167 0003321 212.4997 147.6021 15.60813985642873
| Epoch (UTC): | 22 December 2024 20:49:40 |
| Eccentricity: | 0.0003321 |
| inclination: | 74.7210° |
| perigee height: | 383 km |
| apogee height: | 387 km |
| right ascension of ascending node: | 266.8167° |
| argument of perigee: | 212.4997° |
| revolutions per day: | 15.60813985 |
| mean anomaly at epoch: | 147.6021° |
| orbit number at epoch: | 64287 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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