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 59463U 26145.51050164 +.00000000 +00000-0 +90164-4 0 00004
2 59463 43.0016 317.0301 0001231 269.3639 90.7071 15.27578754 08
| Epoch (UTC): | 25 May 2026 12:15:07 |
| Eccentricity: | 0.0001231 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 317.0301° |
| argument of perigee: | 269.3639° |
| revolutions per day: | 15.27578754 |
| mean anomaly at epoch: | 90.7071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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