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 31574U 26145.30892764 +.00000000 +00000-0 +20530-3 0 00003
2 31574 51.9897 161.1543 0001368 265.8419 107.4396 11.91658308 07
| Epoch (UTC): | 25 May 2026 07:24:51 |
| Eccentricity: | 0.0001368 |
| inclination: | 51.9897° |
| perigee height: | 1717 km |
| apogee height: | 1720 km |
| right ascension of ascending node: | 161.1543° |
| argument of perigee: | 265.8419° |
| revolutions per day: | 11.91658308 |
| mean anomaly at epoch: | 107.4396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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