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 67380U 26145.58335647 +.00000000 +00000-0 -48203-2 0 00006
2 67380 97.8000 144.5358 0000139 350.0968 32.3904 14.86004910 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000139 |
| inclination: | 97.8000° |
| perigee height: | 610 km |
| apogee height: | 611 km |
| right ascension of ascending node: | 144.5358° |
| argument of perigee: | 350.0968° |
| revolutions per day: | 14.86004910 |
| mean anomaly at epoch: | 32.3904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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