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 67847U 26145.55675892 +.00000000 +00000-0 +58672-3 0 00001
2 67847 43.0020 178.4346 0002035 285.4557 74.6070 15.28430957 00
| Epoch (UTC): | 25 May 2026 13:21:43 |
| Eccentricity: | 0.0002035 |
| inclination: | 43.0020° |
| perigee height: | 479 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 178.4346° |
| argument of perigee: | 285.4557° |
| revolutions per day: | 15.28430957 |
| mean anomaly at epoch: | 74.6070° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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