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 56034U 26144.93688795 +.00000000 +00000-0 +17265-4 0 00008
2 56034 43.0039 334.8565 0001432 270.5646 89.5042 15.27573935 08
| Epoch (UTC): | 24 May 2026 22:29:07 |
| Eccentricity: | 0.0001432 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 334.8565° |
| argument of perigee: | 270.5646° |
| revolutions per day: | 15.27573935 |
| mean anomaly at epoch: | 89.5042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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