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 46033U 26145.22814148 +.00000000 +00000-0 +54059-4 0 00004
2 46033 53.1601 131.2004 0001600 111.3275 248.7896 15.30196819 09
| Epoch (UTC): | 25 May 2026 05:28:31 |
| Eccentricity: | 0.0001600 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 131.2004° |
| argument of perigee: | 111.3275° |
| revolutions per day: | 15.30196819 |
| mean anomaly at epoch: | 248.7896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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