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 39444U 13066AE 25137.63239965 .00009863 00000-0 74185-3 0 9995
2 39444 97.7830 99.4635 0043478 103.6144 256.9928 15.01990334620140
| Epoch (UTC): | 17 May 2025 15:10:39 |
| Eccentricity: | 0.0043478 |
| inclination: | 97.7830° |
| perigee height: | 530 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 99.4635° |
| argument of perigee: | 103.6144° |
| revolutions per day: | 15.01990334 |
| mean anomaly at epoch: | 256.9928° |
| orbit number at epoch: | 62014 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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