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 46955U 26145.59802145 +.00000000 +00000-0 +28563-3 0 00001
2 46955 97.5815 339.9086 0004052 4.4422 355.6875 15.69339638 03
| Epoch (UTC): | 25 May 2026 14:21:09 |
| Eccentricity: | 0.0004052 |
| inclination: | 97.5815° |
| perigee height: | 358 km |
| apogee height: | 364 km |
| right ascension of ascending node: | 339.9086° |
| argument of perigee: | 4.4422° |
| revolutions per day: | 15.69339638 |
| mean anomaly at epoch: | 355.6875° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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