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 55422U 26145.58353051 +.00000000 +00000-0 +32442-4 0 00008
2 55422 69.9991 250.4302 0003544 269.0412 91.0341 14.98333303 04
| Epoch (UTC): | 25 May 2026 14:00:17 |
| Eccentricity: | 0.0003544 |
| inclination: | 69.9991° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 250.4302° |
| argument of perigee: | 269.0412° |
| revolutions per day: | 14.98333303 |
| mean anomaly at epoch: | 91.0341° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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