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 56370U 26145.14350259 +.00000000 +00000-0 +00000-0 0 00001
2 56370 0.0137 321.8091 0000845 118.5113 125.1610 1.00270815 05
| Epoch (UTC): | 25 May 2026 03:26:38 |
| Eccentricity: | 0.0000845 |
| inclination: | 0.0137° |
| perigee height: | 35783 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 321.8091° |
| argument of perigee: | 118.5113° |
| revolutions per day: | 1.00270815 |
| mean anomaly at epoch: | 125.1610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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