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 46232U 26145.60329992 +.00000000 +00000-0 +30700-3 0 00001
2 46232 97.2104 186.4927 0008886 164.7879 195.3632 15.31560841 04
| Epoch (UTC): | 25 May 2026 14:28:45 |
| Eccentricity: | 0.0008886 |
| inclination: | 97.2104° |
| perigee height: | 465 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 186.4927° |
| argument of perigee: | 164.7879° |
| revolutions per day: | 15.31560841 |
| mean anomaly at epoch: | 195.3632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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