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 56298U 26145.46643141 +.00000000 +00000-0 +30538-4 0 00003
2 56298 43.0009 135.1116 0000997 270.5042 89.5695 15.27578953 05
| Epoch (UTC): | 25 May 2026 11:11:39 |
| Eccentricity: | 0.0000997 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.1116° |
| argument of perigee: | 270.5042° |
| revolutions per day: | 15.27578953 |
| mean anomaly at epoch: | 89.5695° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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