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 56698U 26145.55116557 +.00000000 +00000-0 -15697-5 0 00004
2 56698 43.0035 185.8157 0001736 275.8581 84.2073 15.27576721 06
| Epoch (UTC): | 25 May 2026 13:13:40 |
| Eccentricity: | 0.0001736 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.8157° |
| argument of perigee: | 275.8581° |
| revolutions per day: | 15.27576721 |
| mean anomaly at epoch: | 84.2073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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