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 56297U 26145.42674455 +.00000000 +00000-0 +45506-4 0 00001
2 56297 43.0044 135.6659 0001328 276.6511 83.4189 15.27578671 05
| Epoch (UTC): | 25 May 2026 10:14:30 |
| Eccentricity: | 0.0001328 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.6659° |
| argument of perigee: | 276.6511° |
| revolutions per day: | 15.27578671 |
| mean anomaly at epoch: | 83.4189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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