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 46029U 26107.83543856 +.00000000 +00000-0 +67136-4 0 00009
2 46029 53.1588 304.8844 0001014 91.1275 268.9842 15.30196165 01
| Epoch (UTC): | 17 April 2026 20:03:01 |
| Eccentricity: | 0.0001014 |
| inclination: | 53.1588° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 304.8844° |
| argument of perigee: | 91.1275° |
| revolutions per day: | 15.30196165 |
| mean anomaly at epoch: | 268.9842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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