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 45406U 26145.22857027 +.00000000 +00000-0 +12799-2 0 00003
2 45406 53.1559 132.1770 0005528 29.0666 331.0644 15.36614893 06
| Epoch (UTC): | 25 May 2026 05:29:08 |
| Eccentricity: | 0.0005528 |
| inclination: | 53.1559° |
| perigee height: | 452 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 132.1770° |
| argument of perigee: | 29.0666° |
| revolutions per day: | 15.36614893 |
| mean anomaly at epoch: | 331.0644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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