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 67891U 26145.55748318 +.00000000 +00000-0 +87436-3 0 00004
2 67891 97.2854 78.0977 0001280 87.0581 273.0809 15.33456056 03
| Epoch (UTC): | 25 May 2026 13:22:46 |
| Eccentricity: | 0.0001280 |
| inclination: | 97.2854° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 78.0977° |
| argument of perigee: | 87.0581° |
| revolutions per day: | 15.33456056 |
| mean anomaly at epoch: | 273.0809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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