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 41174U 26105.27421623 +.00000000 +00000-0 +00000-0 0 00001
2 41174 55.7884 102.9858 0005614 326.9879 33.0027 1.70474182 08
| Epoch (UTC): | 15 April 2026 06:34:52 |
| Eccentricity: | 0.0005614 |
| inclination: | 55.7884° |
| perigee height: | 23206 km |
| apogee height: | 23239 km |
| right ascension of ascending node: | 102.9858° |
| argument of perigee: | 326.9879° |
| revolutions per day: | 1.70474182 |
| mean anomaly at epoch: | 33.0027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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