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 67774U 26145.58335647 +.00000000 +00000-0 +20625-2 0 00000
2 67774 51.8831 207.3869 0003201 310.7524 4.6505 15.28082556 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0003201 |
| inclination: | 51.8831° |
| perigee height: | 479 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 207.3869° |
| argument of perigee: | 310.7524° |
| revolutions per day: | 15.28082556 |
| mean anomaly at epoch: | 4.6505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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