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 56035U 26145.57276388 +.00000000 +00000-0 +27814-4 0 00002
2 56035 43.0055 331.0340 0001499 279.7742 80.2940 15.27571817 00
| Epoch (UTC): | 25 May 2026 13:44:46 |
| Eccentricity: | 0.0001499 |
| inclination: | 43.0055° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.0340° |
| argument of perigee: | 279.7742° |
| revolutions per day: | 15.27571817 |
| mean anomaly at epoch: | 80.2940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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