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 59232U 26145.48742771 +.00000000 +00000-0 +21015-4 0 00005
2 59232 42.9996 69.6053 0000737 273.1948 86.8820 15.27574846 03
| Epoch (UTC): | 25 May 2026 11:41:53 |
| Eccentricity: | 0.0000737 |
| inclination: | 42.9996° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.6053° |
| argument of perigee: | 273.1948° |
| revolutions per day: | 15.27574846 |
| mean anomaly at epoch: | 86.8820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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