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 56413U 26145.28463683 +.00000000 +00000-0 +81950-5 0 00008
2 56413 43.0017 114.9079 0000714 286.7709 73.3064 15.27571861 04
| Epoch (UTC): | 25 May 2026 06:49:52 |
| Eccentricity: | 0.0000714 |
| inclination: | 43.0017° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 114.9079° |
| argument of perigee: | 286.7709° |
| revolutions per day: | 15.27571861 |
| mean anomaly at epoch: | 73.3064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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