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 67365U 26145.26075832 +.00000000 +00000-0 +46237-3 0 00006
2 67365 97.7990 144.1727 0007432 205.6520 154.4329 14.88297877 01
| Epoch (UTC): | 25 May 2026 06:15:29 |
| Eccentricity: | 0.0007432 |
| inclination: | 97.7990° |
| perigee height: | 598 km |
| apogee height: | 608 km |
| right ascension of ascending node: | 144.1727° |
| argument of perigee: | 205.6520° |
| revolutions per day: | 14.88297877 |
| mean anomaly at epoch: | 154.4329° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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