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 56707U 26145.54729964 +.00000000 +00000-0 +32111-4 0 00004
2 56707 43.0019 197.0750 0001699 254.8071 105.2593 15.27578188 02
| Epoch (UTC): | 25 May 2026 13:08:06 |
| Eccentricity: | 0.0001699 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 197.0750° |
| argument of perigee: | 254.8071° |
| revolutions per day: | 15.27578188 |
| mean anomaly at epoch: | 105.2593° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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