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 56027U 26145.21499197 +.00000000 +00000-0 +94586-5 0 00000
2 56027 43.0043 332.6583 0001253 267.5676 92.5033 15.27577640 02
| Epoch (UTC): | 25 May 2026 05:09:35 |
| Eccentricity: | 0.0001253 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 332.6583° |
| argument of perigee: | 267.5676° |
| revolutions per day: | 15.27577640 |
| mean anomaly at epoch: | 92.5033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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