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 59020U 26145.53628514 +.00000000 +00000-0 +00000-0 0 00001
2 59020 4.2280 326.8173 0004094 107.9069 121.7714 1.00276122 07
| Epoch (UTC): | 25 May 2026 12:52:15 |
| Eccentricity: | 0.0004094 |
| inclination: | 4.2280° |
| perigee height: | 35768 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 326.8173° |
| argument of perigee: | 107.9069° |
| revolutions per day: | 1.00276122 |
| mean anomaly at epoch: | 121.7714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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