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 56898U 26145.03623897 +.00000000 +00000-0 +25975-4 0 00007
2 56898 43.0044 10.8668 0001305 247.3193 112.7521 15.27577899 09
| Epoch (UTC): | 25 May 2026 00:52:11 |
| Eccentricity: | 0.0001305 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 10.8668° |
| argument of perigee: | 247.3193° |
| revolutions per day: | 15.27577899 |
| mean anomaly at epoch: | 112.7521° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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