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 45412U 26145.33512462 +.00000000 +00000-0 +12293-2 0 00002
2 45412 53.1554 131.3881 0006379 29.0956 331.0402 15.36847023 04
| Epoch (UTC): | 25 May 2026 08:02:34 |
| Eccentricity: | 0.0006379 |
| inclination: | 53.1554° |
| perigee height: | 451 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 131.3881° |
| argument of perigee: | 29.0956° |
| revolutions per day: | 15.36847023 |
| mean anomaly at epoch: | 331.0402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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