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 25197.84018793 .00005074 00000-0 37774-3 0 9991
2 39444 97.7846 159.9073 0040602 260.0665 99.5975 15.02741861629778
| Epoch (UTC): | 16 July 2025 20:09:52 |
| Eccentricity: | 0.0040602 |
| inclination: | 97.7846° |
| perigee height: | 530 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 159.9073° |
| argument of perigee: | 260.0665° |
| revolutions per day: | 15.02741861 |
| mean anomaly at epoch: | 99.5975° |
| orbit number at epoch: | 62977 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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