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 67886U 26145.54809964 +.00000000 +00000-0 +98416-3 0 00002
2 67886 97.2858 79.0201 0001902 102.9166 257.2289 15.33481458 09
| Epoch (UTC): | 25 May 2026 13:09:15 |
| Eccentricity: | 0.0001902 |
| inclination: | 97.2858° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 79.0201° |
| argument of perigee: | 102.9166° |
| revolutions per day: | 15.33481458 |
| mean anomaly at epoch: | 257.2289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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