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 56874U 26145.54637963 +.00000000 +00000-0 +45580-3 0 00009
2 56874 49.1069 161.9621 0005917 308.0571 51.9844 15.41392439 05
| Epoch (UTC): | 25 May 2026 13:06:47 |
| Eccentricity: | 0.0005917 |
| inclination: | 49.1069° |
| perigee height: | 438 km |
| apogee height: | 446 km |
| right ascension of ascending node: | 161.9621° |
| argument of perigee: | 308.0571° |
| revolutions per day: | 15.41392439 |
| mean anomaly at epoch: | 51.9844° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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