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 45404U 26145.23272674 +.00000000 +00000-0 +12377-2 0 00003
2 45404 53.1558 132.1305 0006013 37.0683 323.0734 15.36236656 03
| Epoch (UTC): | 25 May 2026 05:35:07 |
| Eccentricity: | 0.0006013 |
| inclination: | 53.1558° |
| perigee height: | 453 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 132.1305° |
| argument of perigee: | 37.0683° |
| revolutions per day: | 15.36236656 |
| mean anomaly at epoch: | 323.0734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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