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 56321U 26145.27654987 +.00000000 +00000-0 +16446-2 0 00009
2 56321 97.4475 146.3844 0001223 112.9770 247.1586 15.05657815 06
| Epoch (UTC): | 25 May 2026 06:38:13 |
| Eccentricity: | 0.0001223 |
| inclination: | 97.4475° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 146.3844° |
| argument of perigee: | 112.9770° |
| revolutions per day: | 15.05657815 |
| mean anomaly at epoch: | 247.1586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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