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 25340.87402311 .00013472 00000-0 91562-3 0 9993
2 39444 97.8053 304.0814 0040280 134.8342 225.6170 15.05808706650685
| Epoch (UTC): | 06 December 2025 20:58:35 |
| Eccentricity: | 0.0040280 |
| inclination: | 97.8053° |
| perigee height: | 521 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 304.0814° |
| argument of perigee: | 134.8342° |
| revolutions per day: | 15.05808706 |
| mean anomaly at epoch: | 225.6170° |
| orbit number at epoch: | 65068 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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