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 56117U 26145.48571804 +.00000000 +00000-0 +12773-4 0 00002
2 56117 43.0032 73.4168 0001212 266.8764 93.1950 15.27580546 08
| Epoch (UTC): | 25 May 2026 11:39:26 |
| Eccentricity: | 0.0001212 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 73.4168° |
| argument of perigee: | 266.8764° |
| revolutions per day: | 15.27580546 |
| mean anomaly at epoch: | 93.1950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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