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 59452U 26145.50200146 +.00000000 +00000-0 +28772-3 0 00003
2 59452 45.4123 1.7889 0007073 292.4387 67.5742 14.98367393 05
| Epoch (UTC): | 25 May 2026 12:02:52 |
| Eccentricity: | 0.0007073 |
| inclination: | 45.4123° |
| perigee height: | 567 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 1.7889° |
| argument of perigee: | 292.4387° |
| revolutions per day: | 14.98367393 |
| mean anomaly at epoch: | 67.5742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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