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 56424U 26145.23087299 +.00000000 +00000-0 +40442-4 0 00000
2 56424 43.0037 107.4628 0001419 269.7175 90.3513 15.26742684 06
| Epoch (UTC): | 25 May 2026 05:32:27 |
| Eccentricity: | 0.0001419 |
| inclination: | 43.0037° |
| perigee height: | 485 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 107.4628° |
| argument of perigee: | 269.7175° |
| revolutions per day: | 15.26742684 |
| mean anomaly at epoch: | 90.3513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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