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 64374U 26145.54235051 +.00000000 +00000-0 +22074-2 0 00007
2 64374 43.0004 340.9066 0002294 251.3218 108.7401 15.70975723 01
| Epoch (UTC): | 25 May 2026 13:00:59 |
| Eccentricity: | 0.0002294 |
| inclination: | 43.0004° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 340.9066° |
| argument of perigee: | 251.3218° |
| revolutions per day: | 15.70975723 |
| mean anomaly at epoch: | 108.7401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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