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 37779U 26155.74985803 +.00000000 +00000-0 +00000-0 0 00009
2 37779 0.6562 84.7219 0003463 342.6358 133.7544 1.00273467 09
| Epoch (UTC): | 04 June 2026 17:59:47 |
| Eccentricity: | 0.0003463 |
| inclination: | 0.6562° |
| perigee height: | 35772 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 84.7219° |
| argument of perigee: | 342.6358° |
| revolutions per day: | 1.00273467 |
| mean anomaly at epoch: | 133.7544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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