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 59235U 26145.50028045 +.00000000 +00000-0 +56478-5 0 00004
2 59235 43.0022 69.7199 0000821 276.8722 83.2036 15.27574432 05
| Epoch (UTC): | 25 May 2026 12:00:24 |
| Eccentricity: | 0.0000821 |
| inclination: | 43.0022° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.7199° |
| argument of perigee: | 276.8722° |
| revolutions per day: | 15.27574432 |
| mean anomaly at epoch: | 83.2036° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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