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 is defined by the following mean orbital elements,
1 12933U 81108A 25310.49239420 .00000119 00000-0 00000-0 0 9991
2 12933 71.5073 119.7468 4749935 327.7124 272.1738 2.00242621321809
| Epoch (UTC): | 06 November 2025 11:49:02 |
| Eccentricity: | 0.4749935 |
| inclination: | 71.5073° |
| perigee height: | 7581 km |
| apogee height: | 32840 km |
| right ascension of ascending node: | 119.7468° |
| argument of perigee: | 327.7124° |
| revolutions per day: | 2.00242621 |
| mean anomaly at epoch: | 272.1738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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