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 46059U 26145.21848429 +.00000000 +00000-0 +12171-4 0 00009
2 46059 53.1595 117.9783 0001001 90.4587 269.6529 15.31704444 07
| Epoch (UTC): | 25 May 2026 05:14:37 |
| Eccentricity: | 0.0001001 |
| inclination: | 53.1595° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 117.9783° |
| argument of perigee: | 90.4587° |
| revolutions per day: | 15.31704444 |
| mean anomaly at epoch: | 269.6529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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