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 01778U 26110.81839138 +.00000000 +00000-0 +53880-4 0 00005
2 01778 34.2536 152.1817 0739466 153.9835 209.9992 13.49765872 04
| Epoch (UTC): | 20 April 2026 19:38:29 |
| Eccentricity: | 0.0739466 |
| inclination: | 34.2536° |
| perigee height: | 522 km |
| apogee height: | 1624 km |
| right ascension of ascending node: | 152.1817° |
| argument of perigee: | 153.9835° |
| revolutions per day: | 13.49765872 |
| mean anomaly at epoch: | 209.9992° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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