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 56899U 26145.31819777 +.00000000 +00000-0 +12936-4 0 00006
2 56899 43.0038 8.6898 0001109 259.8109 100.2618 15.27576518 06
| Epoch (UTC): | 25 May 2026 07:38:12 |
| Eccentricity: | 0.0001109 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 8.6898° |
| argument of perigee: | 259.8109° |
| revolutions per day: | 15.27576518 |
| mean anomaly at epoch: | 100.2618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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