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 46043U 26145.33772502 +.00000000 +00000-0 +29640-4 0 00002
2 46043 53.1585 130.2271 0001351 101.8930 258.2223 15.31698692 08
| Epoch (UTC): | 25 May 2026 08:06:19 |
| Eccentricity: | 0.0001351 |
| inclination: | 53.1585° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 130.2271° |
| argument of perigee: | 101.8930° |
| revolutions per day: | 15.31698692 |
| mean anomaly at epoch: | 258.2223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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