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 12904U 81103B 25343.10567918 .00007488 00000-0 34439-3 0 9996
2 12904 81.1590 319.6094 0011340 226.7698 133.2587 15.20160623959461
| Epoch (UTC): | 09 December 2025 02:32:10 |
| Eccentricity: | 0.0011340 |
| inclination: | 81.1590° |
| perigee height: | 497 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 319.6094° |
| argument of perigee: | 226.7698° |
| revolutions per day: | 15.20160623 |
| mean anomaly at epoch: | 133.2587° |
| orbit number at epoch: | 95946 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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