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 56301U 26145.44463682 +.00000000 +00000-0 +31029-3 0 00001
2 56301 42.9999 135.0078 0001450 267.6522 92.4164 15.27322177 06
| Epoch (UTC): | 25 May 2026 10:40:16 |
| Eccentricity: | 0.0001450 |
| inclination: | 42.9999° |
| perigee height: | 483 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 135.0078° |
| argument of perigee: | 267.6522° |
| revolutions per day: | 15.27322177 |
| mean anomaly at epoch: | 92.4164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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