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 56302U 26145.45744366 +.00000000 +00000-0 +19944-3 0 00006
2 56302 42.9995 135.0417 0000471 204.6405 155.4425 15.27602463 02
| Epoch (UTC): | 25 May 2026 10:58:43 |
| Eccentricity: | 0.0000471 |
| inclination: | 42.9995° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 135.0417° |
| argument of perigee: | 204.6405° |
| revolutions per day: | 15.27602463 |
| mean anomaly at epoch: | 155.4425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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