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 67452U 26145.42980323 +.00000000 +00000-0 +46586-3 0 00008
2 67452 43.0017 132.2711 0001624 267.8762 92.1904 15.27587142 06
| Epoch (UTC): | 25 May 2026 10:18:54 |
| Eccentricity: | 0.0001624 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.2711° |
| argument of perigee: | 267.8762° |
| revolutions per day: | 15.27587142 |
| mean anomaly at epoch: | 92.1904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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