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 56305U 26145.46771248 +.00000000 +00000-0 +83731-4 0 00005
2 56305 42.9993 135.0960 0001063 274.3003 85.7727 15.27582935 03
| Epoch (UTC): | 25 May 2026 11:13:30 |
| Eccentricity: | 0.0001063 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.0960° |
| argument of perigee: | 274.3003° |
| revolutions per day: | 15.27582935 |
| mean anomaly at epoch: | 85.7727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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