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 46159U 26145.64779296 +.00000000 +00000-0 +75618-3 0 00006
2 46159 53.0435 282.0651 0002238 357.0540 3.0463 15.69462618 04
| Epoch (UTC): | 25 May 2026 15:32:49 |
| Eccentricity: | 0.0002238 |
| inclination: | 53.0435° |
| perigee height: | 359 km |
| apogee height: | 362 km |
| right ascension of ascending node: | 282.0651° |
| argument of perigee: | 357.0540° |
| revolutions per day: | 15.69462618 |
| mean anomaly at epoch: | 3.0463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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