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 56414U 26145.38715200 +.00000000 +00000-0 +31415-4 0 00005
2 56414 43.0041 113.9510 0001179 268.8850 91.1867 15.27568651 07
| Epoch (UTC): | 25 May 2026 09:17:29 |
| Eccentricity: | 0.0001179 |
| inclination: | 43.0041° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 113.9510° |
| argument of perigee: | 268.8850° |
| revolutions per day: | 15.27568651 |
| mean anomaly at epoch: | 91.1867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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