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 67584U 26145.58677744 +.00000000 +00000-0 +57919-3 0 00003
2 67584 97.2851 205.9836 0001748 314.6658 45.4442 15.33449422 00
| Epoch (UTC): | 25 May 2026 14:04:57 |
| Eccentricity: | 0.0001748 |
| inclination: | 97.2851° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 205.9836° |
| argument of perigee: | 314.6658° |
| revolutions per day: | 15.33449422 |
| mean anomaly at epoch: | 45.4442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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