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 49175U 26145.55525869 +.00000000 +00000-0 +89485-5 0 00001
2 49175 70.0003 81.8183 0002775 269.4694 90.6146 14.97520952 08
| Epoch (UTC): | 25 May 2026 13:19:34 |
| Eccentricity: | 0.0002775 |
| inclination: | 70.0003° |
| perigee height: | 573 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 81.8183° |
| argument of perigee: | 269.4694° |
| revolutions per day: | 14.97520952 |
| mean anomaly at epoch: | 90.6146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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