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 45417U 26145.12062470 +.00000000 +00000-0 +54685-3 0 00005
2 45417 53.0455 121.5298 0001183 112.2635 247.8504 15.62384481 08
| Epoch (UTC): | 25 May 2026 02:53:41 |
| Eccentricity: | 0.0001183 |
| inclination: | 53.0455° |
| perigee height: | 380 km |
| apogee height: | 382 km |
| right ascension of ascending node: | 121.5298° |
| argument of perigee: | 112.2635° |
| revolutions per day: | 15.62384481 |
| mean anomaly at epoch: | 247.8504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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