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 46112U 26145.60554611 +.00000000 +00000-0 +00000-0 0 00003
2 46112 0.0382 186.6173 0003864 279.6200 104.7728 1.00270057 09
| Epoch (UTC): | 25 May 2026 14:31:59 |
| Eccentricity: | 0.0003864 |
| inclination: | 0.0382° |
| perigee height: | 35771 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 186.6173° |
| argument of perigee: | 279.6200° |
| revolutions per day: | 1.00270057 |
| mean anomaly at epoch: | 104.7728° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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