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 56528U 26145.29245248 +.00000000 +00000-0 +30333-4 0 00009
2 56528 43.0015 143.3842 0001038 270.9017 89.1716 15.27575643 01
| Epoch (UTC): | 25 May 2026 07:01:07 |
| Eccentricity: | 0.0001038 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 143.3842° |
| argument of perigee: | 270.9017° |
| revolutions per day: | 15.27575643 |
| mean anomaly at epoch: | 89.1716° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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