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 59522U 26145.49239036 +.00000000 +00000-0 +64065-3 0 00004
2 59522 42.9989 226.5075 0002142 288.6571 71.4048 15.27584867 06
| Epoch (UTC): | 25 May 2026 11:49:02 |
| Eccentricity: | 0.0002142 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 226.5075° |
| argument of perigee: | 288.6571° |
| revolutions per day: | 15.27584867 |
| mean anomaly at epoch: | 71.4048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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