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 45786U 26145.39570076 +.00000000 +00000-0 +57362-4 0 00005
2 45786 53.1583 194.4283 0001338 85.8317 274.2837 15.31697440 08
| Epoch (UTC): | 25 May 2026 09:29:48 |
| Eccentricity: | 0.0001338 |
| inclination: | 53.1583° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 194.4283° |
| argument of perigee: | 85.8317° |
| revolutions per day: | 15.31697440 |
| mean anomaly at epoch: | 274.2837° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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