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 67654U 26145.37276903 +.00000000 +00000-0 +89268-3 0 00002
2 67654 97.2856 178.6090 0000302 336.8573 23.2656 15.33455893 08
| Epoch (UTC): | 25 May 2026 08:56:47 |
| Eccentricity: | 0.0000302 |
| inclination: | 97.2856° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.6090° |
| argument of perigee: | 336.8573° |
| revolutions per day: | 15.33455893 |
| mean anomaly at epoch: | 23.2656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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