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 26145.26080078 +.00000000 +00000-0 +10207-4 0 00007
2 46029 53.1600 131.0484 0001100 90.2898 269.8229 15.30196161 08
| Epoch (UTC): | 25 May 2026 06:15:33 |
| Eccentricity: | 0.0001100 |
| inclination: | 53.1600° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 131.0484° |
| argument of perigee: | 90.2898° |
| revolutions per day: | 15.30196161 |
| mean anomaly at epoch: | 269.8229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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