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 39446U 13066AG 25341.86875217 .00008498 00000-0 76299-3 0 9996
2 39446 97.8467 292.2152 0049477 236.1769 123.4736 14.95026458648971
| Epoch (UTC): | 07 December 2025 20:51:00 |
| Eccentricity: | 0.0049477 |
| inclination: | 97.8467° |
| perigee height: | 548 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 292.2152° |
| argument of perigee: | 236.1769° |
| revolutions per day: | 14.95026458 |
| mean anomaly at epoch: | 123.4736° |
| orbit number at epoch: | 64897 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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