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 45414U 26145.29057659 +.00000000 +00000-0 +47591-3 0 00001
2 45414 53.0603 109.6046 0006863 14.4850 345.6361 15.66620408 04
| Epoch (UTC): | 25 May 2026 06:58:25 |
| Eccentricity: | 0.0006863 |
| inclination: | 53.0603° |
| perigee height: | 364 km |
| apogee height: | 373 km |
| right ascension of ascending node: | 109.6046° |
| argument of perigee: | 14.4850° |
| revolutions per day: | 15.66620408 |
| mean anomaly at epoch: | 345.6361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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