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 56423U 26145.27315921 +.00000000 +00000-0 -24764-4 0 00009
2 56423 43.0017 106.9197 0000782 246.4611 113.6158 15.26757472 02
| Epoch (UTC): | 25 May 2026 06:33:20 |
| Eccentricity: | 0.0000782 |
| inclination: | 43.0017° |
| perigee height: | 485 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 106.9197° |
| argument of perigee: | 246.4611° |
| revolutions per day: | 15.26757472 |
| mean anomaly at epoch: | 113.6158° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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