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 46790U 26145.58335647 +.00000000 +00000-0 +71008-3 0 00007
2 46790 53.0374 260.6489 0008265 313.8892 55.2280 15.85237840 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0008265 |
| inclination: | 53.0374° |
| perigee height: | 310 km |
| apogee height: | 321 km |
| right ascension of ascending node: | 260.6489° |
| argument of perigee: | 313.8892° |
| revolutions per day: | 15.85237840 |
| mean anomaly at epoch: | 55.2280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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