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 45405U 26145.37442323 +.00000000 +00000-0 +10588-2 0 00001
2 45405 53.1565 132.4636 0004539 51.8580 308.2830 15.33653836 05
| Epoch (UTC): | 25 May 2026 08:59:10 |
| Eccentricity: | 0.0004539 |
| inclination: | 53.1565° |
| perigee height: | 462 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 132.4636° |
| argument of perigee: | 51.8580° |
| revolutions per day: | 15.33653836 |
| mean anomaly at epoch: | 308.2830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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